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 59487U 26145.36806948 +.00000000 +00000-0 +63594-4 0 00009
2 59487 42.9961 266.6152 0000765 302.1198 57.9579 15.27580493 02
| Epoch (UTC): | 25 May 2026 08:50:01 |
| Eccentricity: | 0.0000765 |
| inclination: | 42.9961° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.6152° |
| argument of perigee: | 302.1198° |
| revolutions per day: | 15.27580493 |
| mean anomaly at epoch: | 57.9579° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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