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 60535U 26145.49558985 +.00000000 +00000-0 +30206-3 0 00007
2 60535 97.6850 222.5171 0002717 113.9372 246.2136 14.98866410 00
| Epoch (UTC): | 25 May 2026 11:53:38 |
| Eccentricity: | 0.0002717 |
| inclination: | 97.6850° |
| perigee height: | 569 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 222.5171° |
| argument of perigee: | 113.9372° |
| revolutions per day: | 14.98866410 |
| mean anomaly at epoch: | 246.2136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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