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 65084U 26145.00002315 +.00000000 +00000-0 +57339-3 0 00005
2 65084 53.1588 29.7584 0001136 75.6400 74.3720 15.42136603 07
| Epoch (UTC): | 25 May 2026 00:00:02 |
| Eccentricity: | 0.0001136 |
| inclination: | 53.1588° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 29.7584° |
| argument of perigee: | 75.6400° |
| revolutions per day: | 15.42136603 |
| mean anomaly at epoch: | 74.3720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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