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 64876U 26145.58061419 +.00000000 +00000-0 +41526-4 0 00008
2 64876 98.6014 108.0567 0000416 352.4526 7.6646 14.21482006 03
| Epoch (UTC): | 25 May 2026 13:56:05 |
| Eccentricity: | 0.0000416 |
| inclination: | 98.6014° |
| perigee height: | 820 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 108.0567° |
| argument of perigee: | 352.4526° |
| revolutions per day: | 14.21482006 |
| mean anomaly at epoch: | 7.6646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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