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 64137U 26145.58335647 +.00000000 +00000-0 +26325-2 0 00003
2 64137 42.9878 336.9203 0026639 287.6178 260.6148 15.72078313 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0026639 |
| inclination: | 42.9878° |
| perigee height: | 335 km |
| apogee height: | 371 km |
| right ascension of ascending node: | 336.9203° |
| argument of perigee: | 287.6178° |
| revolutions per day: | 15.72078313 |
| mean anomaly at epoch: | 260.6148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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