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 39216U 26153.30932059 +.00000000 +00000-0 +00000-0 0 00002
2 39216 1.8879 82.7270 0000967 342.4258 66.5097 1.00270466 01
| Epoch (UTC): | 02 June 2026 07:25:25 |
| Eccentricity: | 0.0000967 |
| inclination: | 1.8879° |
| perigee height: | 35783 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 82.7270° |
| argument of perigee: | 342.4258° |
| revolutions per day: | 1.00270466 |
| mean anomaly at epoch: | 66.5097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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