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 36088U 26145.64258684 +.00000000 +00000-0 +63633-4 0 00004
2 36088 98.0044 127.2704 0012321 92.7000 18.4631 14.63665603 05
| Epoch (UTC): | 25 May 2026 15:25:19 |
| Eccentricity: | 0.0012321 |
| inclination: | 98.0044° |
| perigee height: | 673 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 127.2704° |
| argument of perigee: | 92.7000° |
| revolutions per day: | 14.63665603 |
| mean anomaly at epoch: | 18.4631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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