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 49306U 26145.44008470 +.00000000 +00000-0 -15521-3 0 00008
2 49306 87.9150 309.5067 0001948 98.5754 261.5599 13.19724161 06
| Epoch (UTC): | 25 May 2026 10:33:43 |
| Eccentricity: | 0.0001948 |
| inclination: | 87.9150° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5067° |
| argument of perigee: | 98.5754° |
| revolutions per day: | 13.19724161 |
| mean anomaly at epoch: | 261.5599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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