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 23271.67160582 .00000996 00000-0 14032-3 0 9999
2 25861 98.1291 310.2278 0013997 265.6328 94.3284 14.79517382304710
| Epoch (UTC): | 28 September 2023 16:07:06 |
| Eccentricity: | 0.0013997 |
| inclination: | 98.1291° |
| perigee height: | 621 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 310.2278° |
| argument of perigee: | 265.6328° |
| revolutions per day: | 14.79517382 |
| mean anomaly at epoch: | 94.3284° |
| orbit number at epoch: | 30471 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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