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 64283U 26145.65475561 +.00000000 +00000-0 +92159-4 0 00003
2 64283 86.5008 21.1646 0001733 88.6127 271.5205 13.24410402 01
| Epoch (UTC): | 25 May 2026 15:42:50 |
| Eccentricity: | 0.0001733 |
| inclination: | 86.5008° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 21.1646° |
| argument of perigee: | 88.6127° |
| revolutions per day: | 13.24410402 |
| mean anomaly at epoch: | 271.5205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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