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 24276.93063337 .00000295 00000-0 17757-3 0 9990
2 23088 70.9984 88.6411 0003744 334.1947 25.8988 14.14892337572418
| Epoch (UTC): | 02 October 2024 22:20:06 |
| Eccentricity: | 0.0003744 |
| inclination: | 70.9984° |
| perigee height: | 840 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 88.6411° |
| argument of perigee: | 334.1947° |
| revolutions per day: | 14.14892337 |
| mean anomaly at epoch: | 25.8988° |
| orbit number at epoch: | 57241 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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