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 25397U 98043D 24277.99933150 .00000916 00000-0 41804-3 0 9997
2 25397 98.9364 246.4205 0001250 153.3920 206.7322 14.24141883363124
| Epoch (UTC): | 03 October 2024 23:59:02 |
| Eccentricity: | 0.0001250 |
| inclination: | 98.9364° |
| perigee height: | 810 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 246.4205° |
| argument of perigee: | 153.3920° |
| revolutions per day: | 14.24141883 |
| mean anomaly at epoch: | 206.7322° |
| orbit number at epoch: | 36312 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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