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 65305U 26145.58342003 +.00000000 +00000-0 +51891-4 0 00003
2 65305 50.0058 286.9460 0000605 98.4384 261.6557 13.29322572 09
| Epoch (UTC): | 25 May 2026 14:00:07 |
| Eccentricity: | 0.0000605 |
| inclination: | 50.0058° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 286.9460° |
| argument of perigee: | 98.4384° |
| revolutions per day: | 13.29322572 |
| mean anomaly at epoch: | 261.6557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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