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 59588U 26018.92042245 +.00000000 +00000-0 +15802-1 0 00000
2 59588 97.2378 331.2129 0055114 241.3991 118.1620 13.87305157 08
| Epoch (UTC): | 18 January 2026 22:05:24 |
| Eccentricity: | 0.0055114 |
| inclination: | 97.2378° |
| perigee height: | 898 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 331.2129° |
| argument of perigee: | 241.3991° |
| revolutions per day: | 13.87305157 |
| mean anomaly at epoch: | 118.1620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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