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 02413U 66076B 25341.02827572 .00000136 00000-0 18830-3 0 9996
2 02413 88.8483 94.2090 0030540 261.1451 98.6242 13.51841920922690
| Epoch (UTC): | 07 December 2025 00:40:43 |
| Eccentricity: | 0.0030540 |
| inclination: | 88.8483° |
| perigee height: | 1043 km |
| apogee height: | 1088 km |
| right ascension of ascending node: | 94.2090° |
| argument of perigee: | 261.1451° |
| revolutions per day: | 13.51841920 |
| mean anomaly at epoch: | 98.6242° |
| orbit number at epoch: | 92269 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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