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 61609U 26145.46763701 +.00000000 +00000-0 +20992-2 0 00001
2 61609 87.8872 40.7754 0001148 114.4642 245.6605 13.10373482 07
| Epoch (UTC): | 25 May 2026 11:13:23 |
| Eccentricity: | 0.0001148 |
| inclination: | 87.8872° |
| perigee height: | 1221 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7754° |
| argument of perigee: | 114.4642° |
| revolutions per day: | 13.10373482 |
| mean anomaly at epoch: | 245.6605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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