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 24973U 26088.08162883 +.00000000 +00000-0 +61631-3 0 00008
2 24973 82.0115 119.7241 0296097 30.2184 29.0354 14.36021419 04
| Epoch (UTC): | 29 March 2026 01:57:32 |
| Eccentricity: | 0.0296097 |
| inclination: | 82.0115° |
| perigee height: | 560 km |
| apogee height: | 983 km |
| right ascension of ascending node: | 119.7241° |
| argument of perigee: | 30.2184° |
| revolutions per day: | 14.36021419 |
| mean anomaly at epoch: | 29.0354° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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