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 62894U 26145.32765362 +.00000000 +00000-0 -88586-3 0 00003
2 62894 43.0036 252.8219 0002492 289.7249 70.3334 15.27568089 05
| Epoch (UTC): | 25 May 2026 07:51:49 |
| Eccentricity: | 0.0002492 |
| inclination: | 43.0036° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 252.8219° |
| argument of perigee: | 289.7249° |
| revolutions per day: | 15.27568089 |
| mean anomaly at epoch: | 70.3334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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