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 60537U 26145.43896823 +.00000000 +00000-0 +14115-3 0 00000
2 60537 97.6745 220.3541 0003651 102.1253 258.0378 14.96575924 02
| Epoch (UTC): | 25 May 2026 10:32:06 |
| Eccentricity: | 0.0003651 |
| inclination: | 97.6745° |
| perigee height: | 575 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 220.3541° |
| argument of perigee: | 102.1253° |
| revolutions per day: | 14.96575924 |
| mean anomaly at epoch: | 258.0378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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