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 36508U 26048.16067183 +.00000000 +00000-0 +73466-4 0 00007
2 36508 92.0221 248.2316 0002326 81.8453 278.3018 14.51908985 07
| Epoch (UTC): | 17 February 2026 03:51:22 |
| Eccentricity: | 0.0002326 |
| inclination: | 92.0221° |
| perigee height: | 718 km |
| apogee height: | 721 km |
| right ascension of ascending node: | 248.2316° |
| argument of perigee: | 81.8453° |
| revolutions per day: | 14.51908985 |
| mean anomaly at epoch: | 278.3018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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