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 60485U 26145.44527619 +.00000000 +00000-0 +24397-3 0 00000
2 60485 97.3817 226.4628 0002863 29.4288 330.7114 15.32366450 06
| Epoch (UTC): | 25 May 2026 10:41:11 |
| Eccentricity: | 0.0002863 |
| inclination: | 97.3817° |
| perigee height: | 467 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 226.4628° |
| argument of perigee: | 29.4288° |
| revolutions per day: | 15.32366450 |
| mean anomaly at epoch: | 330.7114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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