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 61860U 26145.34662520 +.00000000 +00000-0 +16554-3 0 00004
2 61860 43.0006 161.4085 0001179 283.9518 76.1202 15.27582995 06
| Epoch (UTC): | 25 May 2026 08:19:08 |
| Eccentricity: | 0.0001179 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 161.4085° |
| argument of perigee: | 283.9518° |
| revolutions per day: | 15.27582995 |
| mean anomaly at epoch: | 76.1202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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