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 51965U 26145.43684530 +.00000000 +00000-0 +20511-4 0 00003
2 51965 53.1630 40.2760 0001319 90.9469 269.1684 15.31696192 05
| Epoch (UTC): | 25 May 2026 10:29:03 |
| Eccentricity: | 0.0001319 |
| inclination: | 53.1630° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 40.2760° |
| argument of perigee: | 90.9469° |
| revolutions per day: | 15.31696192 |
| mean anomaly at epoch: | 269.1684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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