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 60246U 26145.32830686 +.00000000 +00000-0 +78829-3 0 00002
2 60246 97.2116 357.5774 0021087 264.2047 95.6804 15.55834041 05
| Epoch (UTC): | 25 May 2026 07:52:45 |
| Eccentricity: | 0.0021087 |
| inclination: | 97.2116° |
| perigee height: | 385 km |
| apogee height: | 414 km |
| right ascension of ascending node: | 357.5774° |
| argument of perigee: | 264.2047° |
| revolutions per day: | 15.55834041 |
| mean anomaly at epoch: | 95.6804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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