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 60522U 26145.59152635 +.00000000 +00000-0 +17604-3 0 00003
2 60522 97.3840 224.0831 0007646 54.8004 305.3948 15.23748643 07
| Epoch (UTC): | 25 May 2026 14:11:47 |
| Eccentricity: | 0.0007646 |
| inclination: | 97.3840° |
| perigee height: | 489 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 224.0831° |
| argument of perigee: | 54.8004° |
| revolutions per day: | 15.23748643 |
| mean anomaly at epoch: | 305.3948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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