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 64358U 26145.38492291 +.00000000 +00000-0 +17961-3 0 00002
2 64358 70.0007 200.9315 0003975 265.7481 94.3224 14.98335242 04
| Epoch (UTC): | 25 May 2026 09:14:17 |
| Eccentricity: | 0.0003975 |
| inclination: | 70.0007° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 200.9315° |
| argument of perigee: | 265.7481° |
| revolutions per day: | 14.98335242 |
| mean anomaly at epoch: | 94.3224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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