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 61593U 26145.49976815 +.00000000 +00000-0 +63376-4 0 00003
2 61593 53.1613 65.4128 0001246 93.7926 266.3219 15.34374495 04
| Epoch (UTC): | 25 May 2026 11:59:39 |
| Eccentricity: | 0.0001246 |
| inclination: | 53.1613° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 65.4128° |
| argument of perigee: | 93.7926° |
| revolutions per day: | 15.34374495 |
| mean anomaly at epoch: | 266.3219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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