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 59800U 26145.44856019 +.00000000 +00000-0 -93614-4 0 00008
2 59800 43.0023 135.4887 0001632 272.2135 87.8530 15.27553956 05
| Epoch (UTC): | 25 May 2026 10:45:55 |
| Eccentricity: | 0.0001632 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.4887° |
| argument of perigee: | 272.2135° |
| revolutions per day: | 15.27553956 |
| mean anomaly at epoch: | 87.8530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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