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 61667U 26145.30297641 +.00000000 +00000-0 +78205-5 0 00006
2 61667 53.1608 95.3463 0001200 100.4058 259.7078 15.30189248 01
| Epoch (UTC): | 25 May 2026 07:16:17 |
| Eccentricity: | 0.0001200 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.3463° |
| argument of perigee: | 100.4058° |
| revolutions per day: | 15.30189248 |
| mean anomaly at epoch: | 259.7078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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