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 64792U 26145.38609198 +.00000000 +00000-0 +29485-3 0 00004
2 64792 70.0002 301.0189 0002804 264.2823 95.8017 14.98339358 05
| Epoch (UTC): | 25 May 2026 09:15:58 |
| Eccentricity: | 0.0002804 |
| inclination: | 70.0002° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 301.0189° |
| argument of perigee: | 264.2823° |
| revolutions per day: | 14.98339358 |
| mean anomaly at epoch: | 95.8017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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