THE ARAB SATELLITE 813 is a payload in SSO orbit, operated by United Arab Emirates Space Agency / UAE University NSSTC, launched 2025.
| Orbit class | SSO |
| Inclination | 97.6321° |
| Eccentricity | 0.0013097 |
| Period | 95.6 min |
| Apogee | 555 km |
| Perigee | 537 km |
| Mean motion | 15.06683945 rev/day |
| RAAN | 263.7458° |
| Arg of perigee | 292.7342° |
| Mean anomaly | 67.2501° |
| B* | 2.3968e-4 |
| Rev at epoch | 3,145 |
1 66994U 25292B 26188.15281286 .00003501 00000-0 23968-3 0 99922 66994 97.6321 263.7458 0013097 292.7342 67.2501 15.06683945 31459{
"OBJECT_NAME": "THE ARAB SATELLITE 813",
"OBJECT_ID": "2025-292B",
"EPOCH": "2026-07-07T03:40:03.031+00:00",
"MEAN_MOTION": 15.06683945,
"ECCENTRICITY": 0.0013097,
"INCLINATION": 97.6321,
"RA_OF_ASC_NODE": 263.7458,
"ARG_OF_PERICENTER": 292.7342,
"MEAN_ANOMALY": 67.2501,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 66994,
"REV_AT_EPOCH": 3145,
"BSTAR": 0.00023968,
"MEAN_MOTION_DOT": 0.00003501,
"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 | THE ARAB SATELLITE 813 |
| Operator | United Arab Emirates Space Agency / UAE University NSSTCHIGHvia GCAT — Jonathan McDowell's General Catalog |
| Country | United Arab Emirates |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class | PAYLOADHIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |