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 36588U 26145.47835887 +.00000000 +00000-0 +15287-3 0 00007
2 36588 100.4284 333.5197 0016938 328.5742 59.2620 13.16051739 00
| Epoch (UTC): | 25 May 2026 11:28:50 |
| Eccentricity: | 0.0016938 |
| inclination: | 100.4284° |
| perigee height: | 1187 km |
| apogee height: | 1213 km |
| right ascension of ascending node: | 333.5197° |
| argument of perigee: | 328.5742° |
| revolutions per day: | 13.16051739 |
| mean anomaly at epoch: | 59.2620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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