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 59805U 26145.53350838 +.00000000 +00000-0 +31071-3 0 00008
2 59805 97.3876 216.9218 0003187 277.8942 82.1930 15.16430557 06
| Epoch (UTC): | 25 May 2026 12:48:15 |
| Eccentricity: | 0.0003187 |
| inclination: | 97.3876° |
| perigee height: | 514 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 216.9218° |
| argument of perigee: | 277.8942° |
| revolutions per day: | 15.16430557 |
| mean anomaly at epoch: | 82.1930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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