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 02825U 26070.82651919 +.00000000 +00000-0 +70679-4 0 00009
2 02825 69.9705 282.5649 0009586 290.2489 69.7587 13.97709453 03
| Epoch (UTC): | 11 March 2026 19:50:11 |
| Eccentricity: | 0.0009586 |
| inclination: | 69.9705° |
| perigee height: | 895 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 282.5649° |
| argument of perigee: | 290.2489° |
| revolutions per day: | 13.97709453 |
| mean anomaly at epoch: | 69.7587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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