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 26064.76968931 +.00000000 +00000-0 +23997-3 0 00008
2 36088 97.9973 48.7434 0010934 356.7812 126.7048 14.63562566 02
| Epoch (UTC): | 05 March 2026 18:28:21 |
| Eccentricity: | 0.0010934 |
| inclination: | 97.9973° |
| perigee height: | 674 km |
| apogee height: | 689 km |
| right ascension of ascending node: | 48.7434° |
| argument of perigee: | 356.7812° |
| revolutions per day: | 14.63562566 |
| mean anomaly at epoch: | 126.7048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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