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 23088U 94023B 24282.58645293 .00000197 00000-0 12686-3 0 9992
2 23088 70.9995 76.7650 0004166 326.4199 33.6659 14.14895461572946
| Epoch (UTC): | 08 October 2024 14:04:29 |
| Eccentricity: | 0.0004166 |
| inclination: | 70.9995° |
| perigee height: | 839 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 76.7650° |
| argument of perigee: | 326.4199° |
| revolutions per day: | 14.14895461 |
| mean anomaly at epoch: | 33.6659° |
| orbit number at epoch: | 57294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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