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 49208U 26145.32081042 +.00000000 +00000-0 +22440-3 0 00009
2 49208 87.9174 278.9957 0001777 98.8375 261.2960 13.20772331 05
| Epoch (UTC): | 25 May 2026 07:41:58 |
| Eccentricity: | 0.0001777 |
| inclination: | 87.9174° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9957° |
| argument of perigee: | 98.8375° |
| revolutions per day: | 13.20772331 |
| mean anomaly at epoch: | 261.2960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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