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 40111U 26145.60976102 +.00000000 +00000-0 +14627-3 0 00002
2 40111 63.3781 77.9181 0388194 14.9611 346.2522 13.45448354 00
| Epoch (UTC): | 25 May 2026 14:38:03 |
| Eccentricity: | 0.0388194 |
| inclination: | 63.3781° |
| perigee height: | 799 km |
| apogee height: | 1379 km |
| right ascension of ascending node: | 77.9181° |
| argument of perigee: | 14.9611° |
| revolutions per day: | 13.45448354 |
| mean anomaly at epoch: | 346.2522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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