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 07318U 26121.93735215 +.00000000 +00000-0 +00000-0 0 00009
2 07318 2.0576 249.3620 0029065 346.3456 84.6957 1.01977724 07
| Epoch (UTC): | 01 May 2026 22:29:47 |
| Eccentricity: | 0.0029065 |
| inclination: | 2.0576° |
| perigee height: | 35194 km |
| apogee height: | 35436 km |
| right ascension of ascending node: | 249.3620° |
| argument of perigee: | 346.3456° |
| revolutions per day: | 1.01977724 |
| mean anomaly at epoch: | 84.6957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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