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 66398U 26145.38432203 +.00000000 +00000-0 +55693-3 0 00009
2 66398 53.1591 220.2213 0000732 96.6394 263.4692 15.34405758 03
| Epoch (UTC): | 25 May 2026 09:13:25 |
| Eccentricity: | 0.0000732 |
| inclination: | 53.1591° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 220.2213° |
| argument of perigee: | 96.6394° |
| revolutions per day: | 15.34405758 |
| mean anomaly at epoch: | 263.4692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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