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 25979U 99064C 24281.35992884 .00037079 00000-0 21137-2 0 9997
2 25979 98.2368 305.9458 0007958 70.5815 289.6273 15.12658977349845
| Epoch (UTC): | 07 October 2024 08:38:17 |
| Eccentricity: | 0.0007958 |
| inclination: | 98.2368° |
| perigee height: | 522 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 305.9458° |
| argument of perigee: | 70.5815° |
| revolutions per day: | 15.12658977 |
| mean anomaly at epoch: | 289.6273° |
| orbit number at epoch: | 34984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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