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 67870U 26145.60659751 +.00000000 +00000-0 +49340-3 0 00001
2 67870 53.1568 206.8541 0000991 100.2379 259.8733 15.30211693 03
| Epoch (UTC): | 25 May 2026 14:33:30 |
| Eccentricity: | 0.0000991 |
| inclination: | 53.1568° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 206.8541° |
| argument of perigee: | 100.2379° |
| revolutions per day: | 15.30211693 |
| mean anomaly at epoch: | 259.8733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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