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 10677U 26075.63690197 +.00000000 +00000-0 +78560-4 0 00005
2 10677 74.0387 155.1379 0014406 168.1266 192.0232 14.41716674 08
| Epoch (UTC): | 16 March 2026 15:17:08 |
| Eccentricity: | 0.0014406 |
| inclination: | 74.0387° |
| perigee height: | 743 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 155.1379° |
| argument of perigee: | 168.1266° |
| revolutions per day: | 14.41716674 |
| mean anomaly at epoch: | 192.0232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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