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 26106.72339274 +.00000000 +00000-0 +23990-4 0 00003
2 10677 74.0359 97.5429 0013462 99.1262 261.1417 14.41730283 07
| Epoch (UTC): | 16 April 2026 17:21:41 |
| Eccentricity: | 0.0013462 |
| inclination: | 74.0359° |
| perigee height: | 743 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 97.5429° |
| argument of perigee: | 99.1262° |
| revolutions per day: | 14.41730283 |
| mean anomaly at epoch: | 261.1417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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