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 64298U 26145.33237183 +.00000000 +00000-0 +29924-3 0 00009
2 64298 70.0026 1.0206 0002507 268.0729 92.0143 14.98334213 00
| Epoch (UTC): | 25 May 2026 07:58:36 |
| Eccentricity: | 0.0002507 |
| inclination: | 70.0026° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.0206° |
| argument of perigee: | 268.0729° |
| revolutions per day: | 14.98334213 |
| mean anomaly at epoch: | 92.0143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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