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 27508U 26150.58766954 +.00000000 +00000-0 +00000-0 0 00009
2 27508 7.2388 68.7464 0007393 14.6649 171.9928 0.98295418 02
| Epoch (UTC): | 30 May 2026 14:06:14 |
| Eccentricity: | 0.0007393 |
| inclination: | 7.2388° |
| perigee height: | 36318 km |
| apogee height: | 36382 km |
| right ascension of ascending node: | 68.7464° |
| argument of perigee: | 14.6649° |
| revolutions per day: | 0.98295418 |
| mean anomaly at epoch: | 171.9928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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