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 60121U 26145.45522218 +.00000000 +00000-0 +68516-5 0 00001
2 60121 53.1588 202.5801 0001068 65.7236 294.3894 15.69702241 00
| Epoch (UTC): | 25 May 2026 10:55:31 |
| Eccentricity: | 0.0001068 |
| inclination: | 53.1588° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 202.5801° |
| argument of perigee: | 65.7236° |
| revolutions per day: | 15.69702241 |
| mean anomaly at epoch: | 294.3894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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