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 24797U 97020F 25110.31234929 .00001336 00000-0 26511-3 0 9990
2 24797 86.8997 23.3244 0218481 117.4797 1.8212 14.47202266471411
| Epoch (UTC): | 20 April 2025 07:29:46 |
| Eccentricity: | 0.0218481 |
| inclination: | 86.8997° |
| perigee height: | 579 km |
| apogee height: | 890 km |
| right ascension of ascending node: | 23.3244° |
| argument of perigee: | 117.4797° |
| revolutions per day: | 14.47202266 |
| mean anomaly at epoch: | 1.8212° |
| orbit number at epoch: | 47141 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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