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 26374U 00030A 24280.84344503 .00027670 00000-0 18303-2 0 9991
2 26374 68.9231 64.8116 0524485 88.8268 277.2863 14.36013297232948
| Epoch (UTC): | 06 October 2024 20:14:33 |
| Eccentricity: | 0.0524485 |
| inclination: | 68.9231° |
| perigee height: | 397 km |
| apogee height: | 1147 km |
| right ascension of ascending node: | 64.8116° |
| argument of perigee: | 88.8268° |
| revolutions per day: | 14.36013297 |
| mean anomaly at epoch: | 277.2863° |
| orbit number at epoch: | 23294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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