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 20253U 26087.56975345 +.00000000 +00000-0 +00000-0 0 00002
2 20253 12.4438 351.6472 0008059 356.3586 168.8484 1.00275102 09
| Epoch (UTC): | 28 March 2026 13:40:26 |
| Eccentricity: | 0.0008059 |
| inclination: | 12.4438° |
| perigee height: | 35752 km |
| apogee height: | 35820 km |
| right ascension of ascending node: | 351.6472° |
| argument of perigee: | 356.3586° |
| revolutions per day: | 1.00275102 |
| mean anomaly at epoch: | 168.8484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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