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 36089U 26106.65460718 +.00000000 +00000-0 +33812-4 0 00002
2 36089 98.4531 83.9550 0076905 228.9430 130.5103 14.52365943 08
| Epoch (UTC): | 16 April 2026 15:42:38 |
| Eccentricity: | 0.0076905 |
| inclination: | 98.4531° |
| perigee height: | 663 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 83.9550° |
| argument of perigee: | 228.9430° |
| revolutions per day: | 14.52365943 |
| mean anomaly at epoch: | 130.5103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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