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 27006U 26074.30089955 +.00000000 +00000-0 +32872-4 0 00002
2 27006 99.7687 240.2755 0014142 335.5768 90.4042 13.71092399 00
| Epoch (UTC): | 15 March 2026 07:13:17 |
| Eccentricity: | 0.0014142 |
| inclination: | 99.7687° |
| perigee height: | 985 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 240.2755° |
| argument of perigee: | 335.5768° |
| revolutions per day: | 13.71092399 |
| mean anomaly at epoch: | 90.4042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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