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 61869U 26145.64570729 +.00000000 +00000-0 +46725-3 0 00008
2 61869 97.4207 215.9853 0012692 54.5527 305.6896 15.29350846 02
| Epoch (UTC): | 25 May 2026 15:29:49 |
| Eccentricity: | 0.0012692 |
| inclination: | 97.4207° |
| perigee height: | 469 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 215.9853° |
| argument of perigee: | 54.5527° |
| revolutions per day: | 15.29350846 |
| mean anomaly at epoch: | 305.6896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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