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 60469U 26145.49998058 +.00000000 +00000-0 +39454-3 0 00006
2 60469 97.3687 226.0642 0000665 13.1848 346.9413 15.35288100 04
| Epoch (UTC): | 25 May 2026 11:59:58 |
| Eccentricity: | 0.0000665 |
| inclination: | 97.3687° |
| perigee height: | 460 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 226.0642° |
| argument of perigee: | 13.1848° |
| revolutions per day: | 15.35288100 |
| mean anomaly at epoch: | 346.9413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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