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 62094U 26145.43256442 +.00000000 +00000-0 +23170-2 0 00007
2 62094 42.9986 300.4195 0003844 282.6103 77.4334 15.70992968 08
| Epoch (UTC): | 25 May 2026 10:22:53 |
| Eccentricity: | 0.0003844 |
| inclination: | 42.9986° |
| perigee height: | 353 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 300.4195° |
| argument of perigee: | 282.6103° |
| revolutions per day: | 15.70992968 |
| mean anomaly at epoch: | 77.4334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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