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 60480U 26145.16554843 +.00000000 +00000-0 +40163-3 0 00002
2 60480 97.3724 228.6688 0002623 2.4036 357.7223 15.41014707 09
| Epoch (UTC): | 25 May 2026 03:58:23 |
| Eccentricity: | 0.0002623 |
| inclination: | 97.3724° |
| perigee height: | 441 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 228.6688° |
| argument of perigee: | 2.4036° |
| revolutions per day: | 15.41014707 |
| mean anomaly at epoch: | 357.7223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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