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 60539U 26145.14335921 +.00000000 +00000-0 +23502-3 0 00007
2 60539 97.6759 222.4269 0005992 156.0794 204.0709 14.99799841 05
| Epoch (UTC): | 25 May 2026 03:26:26 |
| Eccentricity: | 0.0005992 |
| inclination: | 97.6759° |
| perigee height: | 563 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 222.4269° |
| argument of perigee: | 156.0794° |
| revolutions per day: | 14.99799841 |
| mean anomaly at epoch: | 204.0709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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