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 26106.23358000 +.00000000 +00000-0 +38588-4 0 00006
2 21152 82.9299 349.7480 0040328 249.1610 231.0214 13.74497777 06
| Epoch (UTC): | 16 April 2026 05:36:21 |
| Eccentricity: | 0.0040328 |
| inclination: | 82.9299° |
| perigee height: | 954 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 349.7480° |
| argument of perigee: | 249.1610° |
| revolutions per day: | 13.74497777 |
| mean anomaly at epoch: | 231.0214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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