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 60944U 26145.34049808 +.00000000 +00000-0 +36497-4 0 00003
2 60944 53.1590 133.8262 0001130 93.5541 266.5589 15.30194826 05
| Epoch (UTC): | 25 May 2026 08:10:19 |
| Eccentricity: | 0.0001130 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.8262° |
| argument of perigee: | 93.5541° |
| revolutions per day: | 15.30194826 |
| mean anomaly at epoch: | 266.5589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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