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 08110U 26087.80312030 +.00000000 +00000-0 +87273-6 0 00006
2 08110 81.3501 200.1859 0032563 236.9007 122.9038 14.11475558 07
| Epoch (UTC): | 28 March 2026 19:16:29 |
| Eccentricity: | 0.0032563 |
| inclination: | 81.3501° |
| perigee height: | 831 km |
| apogee height: | 878 km |
| right ascension of ascending node: | 200.1859° |
| argument of perigee: | 236.9007° |
| revolutions per day: | 14.11475558 |
| mean anomaly at epoch: | 122.9038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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