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 49206U 26145.29470029 +.00000000 +00000-0 +19350-3 0 00006
2 49206 87.9171 340.0107 0001916 91.5220 268.6132 13.18686896 01
| Epoch (UTC): | 25 May 2026 07:04:22 |
| Eccentricity: | 0.0001916 |
| inclination: | 87.9171° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0107° |
| argument of perigee: | 91.5220° |
| revolutions per day: | 13.18686896 |
| mean anomaly at epoch: | 268.6132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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