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 60478U 26145.21335458 +.00000000 +00000-0 +49239-3 0 00007
2 60478 97.3765 229.1020 0003460 4.7702 355.3577 15.40535339 06
| Epoch (UTC): | 25 May 2026 05:07:13 |
| Eccentricity: | 0.0003460 |
| inclination: | 97.3765° |
| perigee height: | 442 km |
| apogee height: | 447 km |
| right ascension of ascending node: | 229.1020° |
| argument of perigee: | 4.7702° |
| revolutions per day: | 15.40535339 |
| mean anomaly at epoch: | 355.3577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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