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 27858U 26150.60029462 +.00000000 +00000-0 +93443-4 0 00003
2 27858 73.9296 206.2849 0008715 274.2134 85.8047 14.81427701 00
| Epoch (UTC): | 30 May 2026 14:24:25 |
| Eccentricity: | 0.0008715 |
| inclination: | 73.9296° |
| perigee height: | 619 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 206.2849° |
| argument of perigee: | 274.2134° |
| revolutions per day: | 14.81427701 |
| mean anomaly at epoch: | 85.8047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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