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 06787U 73054A 24357.63446050 .00000664 00000-0 25694-3 0 9991
2 06787 98.6371 217.6551 0025451 192.7573 167.2970 14.33173380674183
| Epoch (UTC): | 22 December 2024 15:13:37 |
| Eccentricity: | 0.0025451 |
| inclination: | 98.6371° |
| perigee height: | 763 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 217.6551° |
| argument of perigee: | 192.7573° |
| revolutions per day: | 14.33173380 |
| mean anomaly at epoch: | 167.2970° |
| orbit number at epoch: | 67418 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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