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 25316.67957704 .00000157 00000-0 17831-3 0 9999
2 00116 66.8106 60.5919 0069145 62.6887 298.1211 13.92279914266565
| Epoch (UTC): | 12 November 2025 16:18:35 |
| Eccentricity: | 0.0069145 |
| inclination: | 66.8106° |
| perigee height: | 870 km |
| apogee height: | 971 km |
| right ascension of ascending node: | 60.5919° |
| argument of perigee: | 62.6887° |
| revolutions per day: | 13.92279914 |
| mean anomaly at epoch: | 298.1211° |
| orbit number at epoch: | 26656 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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