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 26106.45501843 +.00000000 +00000-0 +10760-3 0 00006
2 21891 19.9942 214.2236 0038303 86.9011 273.5791 14.93587248 04
| Epoch (UTC): | 16 April 2026 10:55:13 |
| Eccentricity: | 0.0038303 |
| inclination: | 19.9942° |
| perigee height: | 560 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 214.2236° |
| argument of perigee: | 86.9011° |
| revolutions per day: | 14.93587248 |
| mean anomaly at epoch: | 273.5791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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