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 25338U 98030A 24261.11245653 .00001025 00000-0 44131-3 0 9997
2 25338 98.5645 286.3057 0011247 60.0786 300.1510 14.26713552370548
| Epoch (UTC): | 17 September 2024 02:41:56 |
| Eccentricity: | 0.0011247 |
| inclination: | 98.5645° |
| perigee height: | 794 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 286.3057° |
| argument of perigee: | 60.0786° |
| revolutions per day: | 14.26713552 |
| mean anomaly at epoch: | 300.1510° |
| orbit number at epoch: | 37054 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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