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 60206U 26145.31475402 +.00000000 +00000-0 +32725-3 0 00003
2 60206 97.2428 356.6848 0015079 317.9255 42.0833 15.42361593 01
| Epoch (UTC): | 25 May 2026 07:33:14 |
| Eccentricity: | 0.0015079 |
| inclination: | 97.2428° |
| perigee height: | 429 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 356.6848° |
| argument of perigee: | 317.9255° |
| revolutions per day: | 15.42361593 |
| mean anomaly at epoch: | 42.0833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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