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 36330U 82025Q 25189.08678270 .00003963 00000-0 15577-2 0 9993
2 36330 82.5315 128.4909 0022813 279.9036 79.9574 14.28971570664793
| Epoch (UTC): | 08 July 2025 02:04:58 |
| Eccentricity: | 0.0022813 |
| inclination: | 82.5315° |
| perigee height: | 779 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 128.4909° |
| argument of perigee: | 279.9036° |
| revolutions per day: | 14.28971570 |
| mean anomaly at epoch: | 79.9574° |
| orbit number at epoch: | 66479 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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