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 65908U 26145.34447128 +.00000000 +00000-0 +54561-3 0 00006
2 65908 53.1595 14.3545 0001381 91.0083 269.1077 15.34410587 04
| Epoch (UTC): | 25 May 2026 08:16:02 |
| Eccentricity: | 0.0001381 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 14.3545° |
| argument of perigee: | 91.0083° |
| revolutions per day: | 15.34410587 |
| mean anomaly at epoch: | 269.1077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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