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 37207U 26145.60554611 +.00000000 +00000-0 +00000-0 0 00008
2 37207 0.0496 240.2197 0000646 276.4938 54.3117 1.00272473 07
| Epoch (UTC): | 25 May 2026 14:31:59 |
| Eccentricity: | 0.0000646 |
| inclination: | 0.0496° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 240.2197° |
| argument of perigee: | 276.4938° |
| revolutions per day: | 1.00272473 |
| mean anomaly at epoch: | 54.3117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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