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 26038.80740316 +.00000000 +00000-0 +11221-2 0 00004
2 36799 98.0620 334.5206 0003074 35.2705 324.8734 15.26176839 09
| Epoch (UTC): | 07 February 2026 19:22:39 |
| Eccentricity: | 0.0003074 |
| inclination: | 98.0620° |
| perigee height: | 485 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 334.5206° |
| argument of perigee: | 35.2705° |
| revolutions per day: | 15.26176839 |
| mean anomaly at epoch: | 324.8734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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