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 60207U 26145.56691789 +.00000000 +00000-0 +33493-3 0 00002
2 60207 97.2401 357.5965 0014450 316.2010 43.8091 15.44125106 01
| Epoch (UTC): | 25 May 2026 13:36:21 |
| Eccentricity: | 0.0014450 |
| inclination: | 97.2401° |
| perigee height: | 424 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 357.5965° |
| argument of perigee: | 316.2010° |
| revolutions per day: | 15.44125106 |
| mean anomaly at epoch: | 43.8091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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