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 62890U 26145.51089451 +.00000000 +00000-0 +19371-2 0 00002
2 62890 42.9996 78.8417 0000683 18.9549 341.1344 15.70899267 08
| Epoch (UTC): | 25 May 2026 12:15:41 |
| Eccentricity: | 0.0000683 |
| inclination: | 42.9996° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 78.8417° |
| argument of perigee: | 18.9549° |
| revolutions per day: | 15.70899267 |
| mean anomaly at epoch: | 341.1344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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