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 64807U 26145.18148014 +.00000000 +00000-0 +28291-3 0 00008
2 64807 70.0002 301.6288 0003249 268.2545 91.8242 14.98337124 02
| Epoch (UTC): | 25 May 2026 04:21:19 |
| Eccentricity: | 0.0003249 |
| inclination: | 70.0002° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 301.6288° |
| argument of perigee: | 268.2545° |
| revolutions per day: | 14.98337124 |
| mean anomaly at epoch: | 91.8242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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