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 28538U 05004B 25198.99502643 -.00000045 00000-0 64714-4 0 9994
2 28538 63.8244 51.0710 0215895 274.0368 83.6011 13.43339379 60256
| Epoch (UTC): | 17 July 2025 23:52:50 |
| Eccentricity: | 0.0215895 |
| inclination: | 63.8244° |
| perigee height: | 935 km |
| apogee height: | 1258 km |
| right ascension of ascending node: | 51.0710° |
| argument of perigee: | 274.0368° |
| revolutions per day: | 13.43339379 |
| mean anomaly at epoch: | 83.6011° |
| orbit number at epoch: | 6025 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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