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 21891U 26041.05373073 +.00000000 +00000-0 +26791-3 0 00003
2 21891 19.9961 305.8155 0038318 346.4294 13.5097 14.93244166 05
| Epoch (UTC): | 10 February 2026 01:17:22 |
| Eccentricity: | 0.0038318 |
| inclination: | 19.9961° |
| perigee height: | 561 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 305.8155° |
| argument of perigee: | 346.4294° |
| revolutions per day: | 14.93244166 |
| mean anomaly at epoch: | 13.5097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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