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 25489U 98055A 23267.94866450 .00001144 00000-0 29215-3 0 9999
2 25489 84.9870 210.2345 0011442 97.3289 262.9214 14.49638690319237
| Epoch (UTC): | 24 September 2023 22:46:04 |
| Eccentricity: | 0.0011442 |
| inclination: | 84.9870° |
| perigee height: | 719 km |
| apogee height: | 735 km |
| right ascension of ascending node: | 210.2345° |
| argument of perigee: | 97.3289° |
| revolutions per day: | 14.49638690 |
| mean anomaly at epoch: | 262.9214° |
| orbit number at epoch: | 31923 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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