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 11111U 26100.16572772 +.00000000 +00000-0 +55379-4 0 00007
2 11111 74.0242 99.8318 0017389 232.9792 126.9770 14.35235174 03
| Epoch (UTC): | 10 April 2026 03:58:38 |
| Eccentricity: | 0.0017389 |
| inclination: | 74.0242° |
| perigee height: | 762 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 99.8318° |
| argument of perigee: | 232.9792° |
| revolutions per day: | 14.35235174 |
| mean anomaly at epoch: | 126.9770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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