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 data is extracted from the following two-line orbital elements,
1 21152U 91019A 25073.60779106 .00000111 00000-0 10171-3 0 9990
2 21152 82.9232 284.6914 0040301 277.8313 135.6099 13.74447695705029
| Epoch (UTC): | 14 March 2025 14:35:13 |
| Eccentricity: | 0.0040301 |
| inclination: | 82.9232° |
| perigee height: | 954 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 284.6914° |
| argument of perigee: | 277.8313° |
| revolutions per day: | 13.74447695 |
| mean anomaly at epoch: | 135.6099° |
| orbit number at epoch: | 70502 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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