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 28651U 05017C 25189.33810968 .00000772 00000-0 10972-3 0 9996
2 28651 97.8880 94.9903 0067467 340.7646 19.1020 14.78263228 84231
| Epoch (UTC): | 08 July 2025 08:06:52 |
| Eccentricity: | 0.0067467 |
| inclination: | 97.8880° |
| perigee height: | 587 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 94.9903° |
| argument of perigee: | 340.7646° |
| revolutions per day: | 14.78263228 |
| mean anomaly at epoch: | 19.1020° |
| orbit number at epoch: | 8423 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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