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 59871U 26145.43445731 +.00000000 +00000-0 -27594-4 0 00004
2 59871 42.9985 197.6263 0000862 297.0825 62.9938 15.27585797 05
| Epoch (UTC): | 25 May 2026 10:25:37 |
| Eccentricity: | 0.0000862 |
| inclination: | 42.9985° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.6263° |
| argument of perigee: | 297.0825° |
| revolutions per day: | 15.27585797 |
| mean anomaly at epoch: | 62.9938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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