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 68361U 26145.15207620 +.00000000 +00000-0 +30375-3 0 00009
2 68361 82.2965 37.9133 0006178 187.4427 172.6753 15.86134355 01
| Epoch (UTC): | 25 May 2026 03:38:59 |
| Eccentricity: | 0.0006178 |
| inclination: | 82.2965° |
| perigee height: | 309 km |
| apogee height: | 317 km |
| right ascension of ascending node: | 37.9133° |
| argument of perigee: | 187.4427° |
| revolutions per day: | 15.86134355 |
| mean anomaly at epoch: | 172.6753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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