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 25255U 26087.95739028 +.00000000 +00000-0 +17934-3 0 00005
2 25255 81.2926 257.4708 0047024 94.0426 30.7007 14.08653412 05
| Epoch (UTC): | 28 March 2026 22:58:38 |
| Eccentricity: | 0.0047024 |
| inclination: | 81.2926° |
| perigee height: | 830 km |
| apogee height: | 898 km |
| right ascension of ascending node: | 257.4708° |
| argument of perigee: | 94.0426° |
| revolutions per day: | 14.08653412 |
| mean anomaly at epoch: | 30.7007° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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