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 116U 61015A 25134.07224617 .00000017 00000-0 71823-4 0 9998
2 116 66.8073 147.3547 0077084 198.1931 161.6389 13.92235253241645
| Epoch (UTC): | 14 May 2025 01:44:02 |
| Eccentricity: | 0.0077084 |
| inclination: | 66.8073° |
| perigee height: | 864 km |
| apogee height: | 977 km |
| right ascension of ascending node: | 147.3547° |
| argument of perigee: | 198.1931° |
| revolutions per day: | 13.92235253 |
| mean anomaly at epoch: | 161.6389° |
| orbit number at epoch: | 24164 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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