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 60200U 26145.53063860 +.00000000 +00000-0 +36019-4 0 00003
2 60200 53.1612 325.3464 0001092 93.1838 266.9288 15.31705454 05
| Epoch (UTC): | 25 May 2026 12:44:07 |
| Eccentricity: | 0.0001092 |
| inclination: | 53.1612° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 325.3464° |
| argument of perigee: | 93.1838° |
| revolutions per day: | 15.31705454 |
| mean anomaly at epoch: | 266.9288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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