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 65427U 26145.54191264 +.00000000 +00000-0 +25490-3 0 00000
2 65427 53.1541 235.1587 0000895 354.6657 5.4334 15.30198443 01
| Epoch (UTC): | 25 May 2026 13:00:21 |
| Eccentricity: | 0.0000895 |
| inclination: | 53.1541° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.1587° |
| argument of perigee: | 354.6657° |
| revolutions per day: | 15.30198443 |
| mean anomaly at epoch: | 5.4334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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