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 25860U 99039A 23155.55898461 .00000742 00000-0 11134-3 0 9999
2 25860 98.0894 202.5715 0001506 72.0923 288.0452 14.77508823285232
| Epoch (UTC): | 04 June 2023 13:24:56 |
| Eccentricity: | 0.0001506 |
| inclination: | 98.0894° |
| perigee height: | 636 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 202.5715° |
| argument of perigee: | 72.0923° |
| revolutions per day: | 14.77508823 |
| mean anomaly at epoch: | 288.0452° |
| orbit number at epoch: | 28523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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