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 25682U 99020A 23030.58073356 .00000641 00000-0 14309-3 0 9999
2 25682 97.9503 74.7184 0001646 90.5866 269.5504 14.59905371265705
| Epoch (UTC): | 30 January 2023 13:56:15 |
| Eccentricity: | 0.0001646 |
| inclination: | 97.9503° |
| perigee height: | 692 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 74.7184° |
| argument of perigee: | 90.5866° |
| revolutions per day: | 14.59905371 |
| mean anomaly at epoch: | 269.5504° |
| orbit number at epoch: | 26570 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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