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 is defined by the following mean orbital elements,
1 12677U 26105.96606213 +.00000000 +00000-0 +00000-0 0 00003
2 12677 8.1160 304.5932 0011148 334.1405 37.9783 0.99554516 03
| Epoch (UTC): | 15 April 2026 23:11:07 |
| Eccentricity: | 0.0011148 |
| inclination: | 8.1160° |
| perigee height: | 35942 km |
| apogee height: | 36036 km |
| right ascension of ascending node: | 304.5932° |
| argument of perigee: | 334.1405° |
| revolutions per day: | 0.99554516 |
| mean anomaly at epoch: | 37.9783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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