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 60526U 26145.13996126 +.00000000 +00000-0 +40772-3 0 00000
2 60526 97.3778 230.9554 0005268 24.4470 335.7026 15.43291121 07
| Epoch (UTC): | 25 May 2026 03:21:32 |
| Eccentricity: | 0.0005268 |
| inclination: | 97.3778° |
| perigee height: | 433 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 230.9554° |
| argument of perigee: | 24.4470° |
| revolutions per day: | 15.43291121 |
| mean anomaly at epoch: | 335.7026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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