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 65945U 26145.47450247 +.00000000 +00000-0 +19065-3 0 00007
2 65945 80.0027 164.6408 0009046 252.9999 107.0239 15.23638799 06
| Epoch (UTC): | 25 May 2026 11:23:17 |
| Eccentricity: | 0.0009046 |
| inclination: | 80.0027° |
| perigee height: | 489 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 164.6408° |
| argument of perigee: | 252.9999° |
| revolutions per day: | 15.23638799 |
| mean anomaly at epoch: | 107.0239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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