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 60122U 26145.58746403 +.00000000 +00000-0 +15153-4 0 00008
2 60122 53.1594 201.9858 0001120 83.3499 276.7646 15.69703547 08
| Epoch (UTC): | 25 May 2026 14:05:56 |
| Eccentricity: | 0.0001120 |
| inclination: | 53.1594° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 201.9858° |
| argument of perigee: | 83.3499° |
| revolutions per day: | 15.69703547 |
| mean anomaly at epoch: | 276.7646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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