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 26906U 26129.72781762 +.00000000 +00000-0 +33163-4 0 00006
2 26906 63.4207 256.6911 0624633 341.7582 16.1904 13.45200937 06
| Epoch (UTC): | 09 May 2026 17:28:03 |
| Eccentricity: | 0.0624633 |
| inclination: | 63.4207° |
| perigee height: | 623 km |
| apogee height: | 1556 km |
| right ascension of ascending node: | 256.6911° |
| argument of perigee: | 341.7582° |
| revolutions per day: | 13.45200937 |
| mean anomaly at epoch: | 16.1904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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