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 25168.12296480 .00000027 00000-0 79341-4 0 9992
2 116 66.8104 64.0481 0074251 174.4647 185.7271 13.92242992246387
| Epoch (UTC): | 17 June 2025 02:57:04 |
| Eccentricity: | 0.0074251 |
| inclination: | 66.8104° |
| perigee height: | 866 km |
| apogee height: | 975 km |
| right ascension of ascending node: | 64.0481° |
| argument of perigee: | 174.4647° |
| revolutions per day: | 13.92242992 |
| mean anomaly at epoch: | 185.7271° |
| orbit number at epoch: | 24638 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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