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 36799U 26102.08019174 +.00000000 +00000-0 +55727-3 0 00007
2 36799 98.0667 42.9209 0004657 106.0924 254.0827 15.29260203 00
| Epoch (UTC): | 12 April 2026 01:55:28 |
| Eccentricity: | 0.0004657 |
| inclination: | 98.0667° |
| perigee height: | 475 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 42.9209° |
| argument of perigee: | 106.0924° |
| revolutions per day: | 15.29260203 |
| mean anomaly at epoch: | 254.0827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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