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 60528U 26145.21621735 +.00000000 +00000-0 +36601-3 0 00008
2 60528 97.3804 228.7754 0006245 33.2563 326.9073 15.38516704 08
| Epoch (UTC): | 25 May 2026 05:11:21 |
| Eccentricity: | 0.0006245 |
| inclination: | 97.3804° |
| perigee height: | 446 km |
| apogee height: | 455 km |
| right ascension of ascending node: | 228.7754° |
| argument of perigee: | 33.2563° |
| revolutions per day: | 15.38516704 |
| mean anomaly at epoch: | 326.9073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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