THEOS-2 (T2V) is a payload in SSO orbit, operated by Geo-Informatics and Space Technology Development Agency, launched 2023.
| Orbit class | SSO |
| Inclination | 97.8872° |
| Eccentricity | 0.0001379 |
| Period | 97.2 min |
| Apogee | 625 km |
| Perigee | 623 km |
| Mean motion | 14.81631173 rev/day |
| RAAN | 258.8514° |
| Arg of perigee | 95.7292° |
| Mean anomaly | 264.4078° |
| B* | 9.2318e-5 |
| Rev at epoch | 14,838 |
1 58016U 23155A 26188.16942627 .00000674 00000-0 92318-4 0 99922 58016 97.8872 258.8514 0001379 95.7292 264.4078 14.81631173148380{
"OBJECT_NAME": "THEOS-2 (T2V)",
"OBJECT_ID": "2023-155A",
"EPOCH": "2026-07-07T04:03:58.43+00:00",
"MEAN_MOTION": 14.81631173,
"ECCENTRICITY": 0.0001379,
"INCLINATION": 97.8872,
"RA_OF_ASC_NODE": 258.8514,
"ARG_OF_PERICENTER": 95.7292,
"MEAN_ANOMALY": 264.4078,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 58016,
"REV_AT_EPOCH": 14838,
"BSTAR": 0.000092318,
"MEAN_MOTION_DOT": 0.00000674,
"MEAN_MOTION_DDOT": 0
}Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.
| Name | THEOS-2 (T2V) |
| Operator | Geo-Informatics and Space Technology Development AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | |
| Launch date | |
| Launch mass (kg) | 417 |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |