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 60946U 26145.63262020 +.00000000 +00000-0 +43157-3 0 00000
2 60946 34.9953 339.8691 0004726 294.4362 65.5860 15.22986265 04
| Epoch (UTC): | 25 May 2026 15:10:58 |
| Eccentricity: | 0.0004726 |
| inclination: | 34.9953° |
| perigee height: | 494 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 339.8691° |
| argument of perigee: | 294.4362° |
| revolutions per day: | 15.22986265 |
| mean anomaly at epoch: | 65.5860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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