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 28415U 04035C 25080.53443439 .00013601 00000-0 57769-3 0 9990
2 28415 97.3914 114.8282 0038747 133.9266 226.5179 15.22484919126062
| Epoch (UTC): | 21 March 2025 12:49:35 |
| Eccentricity: | 0.0038747 |
| inclination: | 97.3914° |
| perigee height: | 472 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 114.8282° |
| argument of perigee: | 133.9266° |
| revolutions per day: | 15.22484919 |
| mean anomaly at epoch: | 226.5179° |
| orbit number at epoch: | 12606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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