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 65089U 26145.41814946 +.00000000 +00000-0 +63735-3 0 00003
2 65089 53.1603 30.5295 0001167 55.6600 304.4511 15.30185907 06
| Epoch (UTC): | 25 May 2026 10:02:08 |
| Eccentricity: | 0.0001167 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 30.5295° |
| argument of perigee: | 55.6600° |
| revolutions per day: | 15.30185907 |
| mean anomaly at epoch: | 304.4511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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