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 64072U 26145.59311920 +.00000000 +00000-0 +17404-2 0 00008
2 64072 42.9996 354.6217 0001622 247.3235 112.7461 15.70881566 04
| Epoch (UTC): | 25 May 2026 14:14:05 |
| Eccentricity: | 0.0001622 |
| inclination: | 42.9996° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 354.6217° |
| argument of perigee: | 247.3235° |
| revolutions per day: | 15.70881566 |
| mean anomaly at epoch: | 112.7461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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