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 60479U 26145.15318116 +.00000000 +00000-0 +21869-3 0 00002
2 60479 97.3749 225.7044 0001972 11.6559 348.4728 15.32344268 01
| Epoch (UTC): | 25 May 2026 03:40:34 |
| Eccentricity: | 0.0001972 |
| inclination: | 97.3749° |
| perigee height: | 467 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 225.7044° |
| argument of perigee: | 11.6559° |
| revolutions per day: | 15.32344268 |
| mean anomaly at epoch: | 348.4728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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