View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 03891U 26032.15481289 +.00000000 +00000-0 +54561-4 0 00000
2 03891 99.6708 269.3968 0038926 224.5902 301.9139 13.42970467 06
| Epoch (UTC): | 01 February 2026 03:42:55 |
| Eccentricity: | 0.0038926 |
| inclination: | 99.6708° |
| perigee height: | 1069 km |
| apogee height: | 1127 km |
| right ascension of ascending node: | 269.3968° |
| argument of perigee: | 224.5902° |
| revolutions per day: | 13.42970467 |
| mean anomaly at epoch: | 301.9139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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