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 44062U 26145.57017780 +.00000000 +00000-0 -88975-4 0 00004
2 44062 87.9003 263.6994 0001770 105.4162 254.7164 13.15549339 00
| Epoch (UTC): | 25 May 2026 13:41:03 |
| Eccentricity: | 0.0001770 |
| inclination: | 87.9003° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.6994° |
| argument of perigee: | 105.4162° |
| revolutions per day: | 13.15549339 |
| mean anomaly at epoch: | 254.7164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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