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 67605U 26145.43704709 +.00000000 +00000-0 +65038-3 0 00004
2 67605 97.2863 210.5294 0001518 92.2352 267.9065 15.33456092 05
| Epoch (UTC): | 25 May 2026 10:29:20 |
| Eccentricity: | 0.0001518 |
| inclination: | 97.2863° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 210.5294° |
| argument of perigee: | 92.2352° |
| revolutions per day: | 15.33456092 |
| mean anomaly at epoch: | 267.9065° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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