| Official name | OBJECT P |
| Alternative name | IRIS-C2 |
| Cospar ID | 2023-174P |
| Norad ID | 58269 |
| Launch date | 2023-11-11 |
| Launch site | AFWTR |
| Launch vehicle | Falcon-9 v1.2 (Block 5) |
| Country/Organization | Taiwan (Republic of China) |
| Type application | Technology |
| Operator | National Cheng Kung University (NCKU) |
| RCS size | MEDIUM |
| Decay date | ON ORBIT |
| Period (min) | 94.77 |
| Inclination (deg) | 97.46 |
| Perigee (km) | 500 |
| Apogee (km) | 516 |
| Eccentricity | 0.015748031496063 |
| Mean motion (revs. per day) | 15.1946818613485 |
| Semi-Major axis (km) | 6886.135 |
| Raan (deg) | 199.8569 |
| Arg of perigee (deg) | 42.1941 |
| Shape | Box |
| Mass (kg) | 3 |
| Height (m) | 0.3 |
| Width (m) | 0.1 |
| Depth (m) | 0.1 |
| Span (m^2) | 0.3 |
| Configuration | CubeSat (3U) |
| Power | 2 deployable, fixed solar arrays, body mounted solar cells, batteries |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| OBJECT P | 2023-174P | 2023-11-11 | AFWTR | Falcon-9 v1.2 (Block 5) | with ICEYE X31, X32, X34, X35, Umbra-SAR 07, 08, Pelican 1, FalconSat 10, SPIP, Aether 1, 2, ION-SCV 013, EPICHyper 3, Intuition 1, Crypto3, Lemur-2 181, OSW Cazorla, Ymir 1, PiCo-IoT 1, ..., 9, Unicorn 2J, 2K, HADES D, ROM 3, SpaceANT-D, Tartan Artibeus 2, Impulse 1, Time We?ll Tell, SpaceVan 001, GHGSat C9, C10, C11, Observer 1A, ProtoMéthée, MANTIS, BRO 10, 11, Connecta T3.1, T3.2, GENMAT 1, NinjaSat, OrbAstro PC1, OrbAstro TR1, PEARL 1C, 1H, Platero, Platform 5, Tiger 5, 6, Vindlér 1, ..., 4, Ella 1, Aman 1 (R), Barry 1, Flock-4q 1, ..., 36, Heron Mk.2, IRIS C2, KAFASAT, Lemur-2 179, 180, OMNI-LER1, Outpost Mission 2, JinjuSat 1, Djibouti 1A, Picacho, Veronika, Hello Test 1, 2 |
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