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 25501U 98058A 23087.63756759 -.00000222 00000-0 00000-0 0 9998
2 25501 9.9808 26.3067 0013596 344.9950 201.8061 0.98178612 88276
| Epoch (UTC): | 28 March 2023 15:18:05 |
| Eccentricity: | 0.0013596 |
| inclination: | 9.9808° |
| perigee height: | 36325 km |
| apogee height: | 36441 km |
| right ascension of ascending node: | 26.3067° |
| argument of perigee: | 344.9950° |
| revolutions per day: | 0.98178612 |
| mean anomaly at epoch: | 201.8061° |
| orbit number at epoch: | 8827 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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