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 24773U 26073.63006595 +.00000000 +00000-0 +78303-4 0 00003
2 24773 82.9250 166.7927 0025442 63.4976 58.1503 13.73972933 00
| Epoch (UTC): | 14 March 2026 15:07:17 |
| Eccentricity: | 0.0025442 |
| inclination: | 82.9250° |
| perigee height: | 967 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 166.7927° |
| argument of perigee: | 63.4976° |
| revolutions per day: | 13.73972933 |
| mean anomaly at epoch: | 58.1503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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