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 27516U 26149.86623405 +.00000000 +00000-0 +00000-0 0 00000
2 27516 11.2179 42.0390 0017113 234.7623 306.7209 0.99273074 00
| Epoch (UTC): | 29 May 2026 20:47:22 |
| Eccentricity: | 0.0017113 |
| inclination: | 11.2179° |
| perigee height: | 35996 km |
| apogee height: | 36142 km |
| right ascension of ascending node: | 42.0390° |
| argument of perigee: | 234.7623° |
| revolutions per day: | 0.99273074 |
| mean anomaly at epoch: | 306.7209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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