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 64958U 26145.65089259 +.00000000 +00000-0 +11753-3 0 00007
2 64958 86.4885 289.9162 0001941 97.1436 262.9919 13.24406687 04
| Epoch (UTC): | 25 May 2026 15:37:17 |
| Eccentricity: | 0.0001941 |
| inclination: | 86.4885° |
| perigee height: | 1166 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 289.9162° |
| argument of perigee: | 97.1436° |
| revolutions per day: | 13.24406687 |
| mean anomaly at epoch: | 262.9919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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