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 58264U 26145.64284933 +.00000000 +00000-0 +17280-3 0 00006
2 58264 97.3907 222.6975 0008655 289.6504 70.3801 15.27097671 07
| Epoch (UTC): | 25 May 2026 15:25:42 |
| Eccentricity: | 0.0008655 |
| inclination: | 97.3907° |
| perigee height: | 479 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 222.6975° |
| argument of perigee: | 289.6504° |
| revolutions per day: | 15.27097671 |
| mean anomaly at epoch: | 70.3801° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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