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 64600U 26145.26525470 +.00000000 +00000-0 +35674-3 0 00006
2 64600 53.1634 339.9275 0001422 90.5595 269.5569 15.30205404 06
| Epoch (UTC): | 25 May 2026 06:21:58 |
| Eccentricity: | 0.0001422 |
| inclination: | 53.1634° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 339.9275° |
| argument of perigee: | 90.5595° |
| revolutions per day: | 15.30205404 |
| mean anomaly at epoch: | 269.5569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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