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 00953U 26088.23323705 +.00000000 +00000-0 +32088-4 0 00004
2 00953 90.0381 192.8157 0030013 311.9895 75.4821 13.58832142 00
| Epoch (UTC): | 29 March 2026 05:35:51 |
| Eccentricity: | 0.0030013 |
| inclination: | 90.0381° |
| perigee height: | 1018 km |
| apogee height: | 1062 km |
| right ascension of ascending node: | 192.8157° |
| argument of perigee: | 311.9895° |
| revolutions per day: | 13.58832142 |
| mean anomaly at epoch: | 75.4821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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