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 25861U 99039B 23152.09284733 .00000545 00000-0 80501-4 0 9993
2 25861 98.1390 189.2102 0014095 293.1657 66.8069 14.79327769287163
| Epoch (UTC): | 01 June 2023 02:13:42 |
| Eccentricity: | 0.0014095 |
| inclination: | 98.1390° |
| perigee height: | 621 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 189.2102° |
| argument of perigee: | 293.1657° |
| revolutions per day: | 14.79327769 |
| mean anomaly at epoch: | 66.8069° |
| orbit number at epoch: | 28716 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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