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 65028U 26145.43036975 +.00000000 +00000-0 +75468-3 0 00002
2 65028 53.1597 297.4289 0001089 102.1822 257.9301 15.30208229 07
| Epoch (UTC): | 25 May 2026 10:19:43 |
| Eccentricity: | 0.0001089 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 297.4289° |
| argument of perigee: | 102.1822° |
| revolutions per day: | 15.30208229 |
| mean anomaly at epoch: | 257.9301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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