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 25940U 99057A 24283.84657515 .00001309 00000-0 46203-3 0 9991
2 25940 98.8189 265.9492 0005435 26.1439 334.0020 14.36453469309159
| Epoch (UTC): | 09 October 2024 20:19:04 |
| Eccentricity: | 0.0005435 |
| inclination: | 98.8189° |
| perigee height: | 766 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 265.9492° |
| argument of perigee: | 26.1439° |
| revolutions per day: | 14.36453469 |
| mean anomaly at epoch: | 334.0020° |
| orbit number at epoch: | 30915 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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