DUBAISAT-1 is a payload in SSO orbit, operated by Emirates Institution for Advanced Science and Technology, launched 2009.
| Orbit class | SSO |
| Inclination | 98.0076° |
| Eccentricity | 0.0010579 |
| Period | 97.6 min |
| Apogee | 652 km |
| Perigee | 637 km |
| Mean motion | 14.75157429 rev/day |
| RAAN | 320.9403° |
| Arg of perigee | 15.3859° |
| Mean anomaly | 344.7669° |
| B* | 1.2535e-4 |
| Rev at epoch | 90,800 |
1 35682U 09041B 26187.89577169 .00000796 00000-0 12535-3 0 99952 35682 98.0076 320.9403 0010579 15.3859 344.7669 14.75157429908001{
"OBJECT_NAME": "DUBAISAT-1",
"OBJECT_ID": "2009-041B",
"EPOCH": "2026-07-06T21:29:54.674+00:00",
"MEAN_MOTION": 14.75157429,
"ECCENTRICITY": 0.0010579,
"INCLINATION": 98.0076,
"RA_OF_ASC_NODE": 320.9403,
"ARG_OF_PERICENTER": 15.3859,
"MEAN_ANOMALY": 344.7669,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 35682,
"REV_AT_EPOCH": 90800,
"BSTAR": 0.00012535,
"MEAN_MOTION_DOT": 0.00000796,
"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 | DUBAISAT-1 |
| Operator | Emirates Institution for Advanced Science and TechnologyHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | United Arab Emirates |
| Launch date | |
| Launch mass (kg) |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |