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 60939U 26145.38892247 +.00000000 +00000-0 +40769-4 0 00001
2 60939 53.1584 133.4217 0001044 84.2278 275.8842 15.30200672 08
| Epoch (UTC): | 25 May 2026 09:20:02 |
| Eccentricity: | 0.0001044 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.4217° |
| argument of perigee: | 84.2278° |
| revolutions per day: | 15.30200672 |
| mean anomaly at epoch: | 275.8842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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