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 37813U 11050A 26010.72733095 0.00006068 00000-0 36733-3 0 02
2 37813 98.0413 192.9031 0002916 212.9103 146.9916 15.10664421 06
| Epoch (UTC): | 10 January 2026 17:27:21 |
| Eccentricity: | 0.0002916 |
| inclination: | 98.0413° |
| perigee height: | 532 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 192.9031° |
| argument of perigee: | 212.9103° |
| revolutions per day: | 15.10664421 |
| mean anomaly at epoch: | 146.9916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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