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 67202U 26145.26957031 +.00000000 +00000-0 +15449-3 0 00007
2 67202 70.0019 341.4510 0002796 267.1267 92.9572 14.98333774 02
| Epoch (UTC): | 25 May 2026 06:28:10 |
| Eccentricity: | 0.0002796 |
| inclination: | 70.0019° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 341.4510° |
| argument of perigee: | 267.1267° |
| revolutions per day: | 14.98333774 |
| mean anomaly at epoch: | 92.9572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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