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 49209U 26145.46162529 +.00000000 +00000-0 +14860-3 0 00002
2 49209 87.9167 339.9803 0001405 85.1645 274.9647 13.18685218 00
| Epoch (UTC): | 25 May 2026 11:04:44 |
| Eccentricity: | 0.0001405 |
| inclination: | 87.9167° |
| perigee height: | 1189 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9803° |
| argument of perigee: | 85.1645° |
| revolutions per day: | 13.18685218 |
| mean anomaly at epoch: | 274.9647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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