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 36869U 26159.02188007 +.00000000 +00000-0 +98615-3 0 00006
2 36869 20.1573 39.3212 4451300 177.6816 185.4643 6.62631933 05
| Epoch (UTC): | 08 June 2026 00:31:30 |
| Eccentricity: | 0.4451300 |
| inclination: | 20.1573° |
| perigee height: | 266 km |
| apogee height: | 10925 km |
| right ascension of ascending node: | 39.3212° |
| argument of perigee: | 177.6816° |
| revolutions per day: | 6.62631933 |
| mean anomaly at epoch: | 185.4643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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