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 00116U 61015A 25140.39391241 .00000029 00000-0 80883-4 0 9997
2 00116 66.8072 131.8878 0076554 193.8753 166.0224 13.92236524242026
| Epoch (UTC): | 20 May 2025 09:27:14 |
| Eccentricity: | 0.0076554 |
| inclination: | 66.8072° |
| perigee height: | 865 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 131.8878° |
| argument of perigee: | 193.8753° |
| revolutions per day: | 13.92236524 |
| mean anomaly at epoch: | 166.0224° |
| orbit number at epoch: | 24202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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