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 21152U 26106.94010880 +.00000000 +00000-0 +38649-4 0 00003
2 21152 82.9298 349.2240 0040338 247.1212 127.1322 13.74497791 02
| Epoch (UTC): | 16 April 2026 22:33:45 |
| Eccentricity: | 0.0040338 |
| inclination: | 82.9298° |
| perigee height: | 954 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 349.2240° |
| argument of perigee: | 247.1212° |
| revolutions per day: | 13.74497791 |
| mean anomaly at epoch: | 127.1322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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