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 64145U 26145.33405975 +.00000000 +00000-0 +74266-3 0 00005
2 64145 43.0057 5.1515 0002585 270.6169 89.4386 15.27628874 07
| Epoch (UTC): | 25 May 2026 08:01:02 |
| Eccentricity: | 0.0002585 |
| inclination: | 43.0057° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 5.1515° |
| argument of perigee: | 270.6169° |
| revolutions per day: | 15.27628874 |
| mean anomaly at epoch: | 89.4386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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