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 64377U 26145.58482422 +.00000000 +00000-0 +13438-2 0 00004
2 64377 42.9984 341.2456 0001266 237.4401 122.6345 15.70927828 08
| Epoch (UTC): | 25 May 2026 14:02:08 |
| Eccentricity: | 0.0001266 |
| inclination: | 42.9984° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 341.2456° |
| argument of perigee: | 237.4401° |
| revolutions per day: | 15.70927828 |
| mean anomaly at epoch: | 122.6345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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