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 60941U 26145.26146554 +.00000000 +00000-0 +11472-4 0 00003
2 60941 53.1593 134.0476 0001123 70.4037 289.7085 15.30195625 07
| Epoch (UTC): | 25 May 2026 06:16:30 |
| Eccentricity: | 0.0001123 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 134.0476° |
| argument of perigee: | 70.4037° |
| revolutions per day: | 15.30195625 |
| mean anomaly at epoch: | 289.7085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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