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 37206U 26065.43538316 +.00000000 +00000-0 +11260-2 0 00005
2 37206 2.2342 96.5311 6900158 324.1861 4.9841 2.77638335 02
| Epoch (UTC): | 06 March 2026 10:26:57 |
| Eccentricity: | 0.6900158 |
| inclination: | 2.2342° |
| perigee height: | 250 km |
| apogee height: | 29761 km |
| right ascension of ascending node: | 96.5311° |
| argument of perigee: | 324.1861° |
| revolutions per day: | 2.77638335 |
| mean anomaly at epoch: | 4.9841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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