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 25343.17222131 .00001491 00000-0 20282-3 0 9993
2 28651 97.8786 245.6188 0066662 200.2146 159.6425 14.78751858106962
| Epoch (UTC): | 09 December 2025 04:07:59 |
| Eccentricity: | 0.0066662 |
| inclination: | 97.8786° |
| perigee height: | 586 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 245.6188° |
| argument of perigee: | 200.2146° |
| revolutions per day: | 14.78751858 |
| mean anomaly at epoch: | 159.6425° |
| orbit number at epoch: | 10696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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