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 64801U 26145.44434691 +.00000000 +00000-0 +27362-3 0 00008
2 64801 70.0000 300.9383 0002749 268.7302 91.3542 14.98335310 05
| Epoch (UTC): | 25 May 2026 10:39:51 |
| Eccentricity: | 0.0002749 |
| inclination: | 70.0000° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 300.9383° |
| argument of perigee: | 268.7302° |
| revolutions per day: | 14.98335310 |
| mean anomaly at epoch: | 91.3542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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