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 61550U 26145.58335647 +.00000000 +00000-0 +66805-1 0 00005
2 61550 53.1598 16.9292 0001066 110.3872 31.6852 15.30781453 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001066 |
| inclination: | 53.1598° |
| perigee height: | 473 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 16.9292° |
| argument of perigee: | 110.3872° |
| revolutions per day: | 15.30781453 |
| mean anomaly at epoch: | 31.6852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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