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 61598U 26145.38822084 +.00000000 +00000-0 -14971-2 0 00000
2 61598 87.8917 25.5974 0001878 61.5531 298.5786 13.11417361 01
| Epoch (UTC): | 25 May 2026 09:19:02 |
| Eccentricity: | 0.0001878 |
| inclination: | 87.8917° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5974° |
| argument of perigee: | 61.5531° |
| revolutions per day: | 13.11417361 |
| mean anomaly at epoch: | 298.5786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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