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 64873U 26145.46075498 +.00000000 +00000-0 +15386-3 0 00008
2 64873 97.6702 209.6701 0004361 34.3969 325.7532 14.93395708 00
| Epoch (UTC): | 25 May 2026 11:03:29 |
| Eccentricity: | 0.0004361 |
| inclination: | 97.6702° |
| perigee height: | 584 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 209.6701° |
| argument of perigee: | 34.3969° |
| revolutions per day: | 14.93395708 |
| mean anomaly at epoch: | 325.7532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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