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 49021U 26145.60550817 +.00000000 +00000-0 -78859-4 0 00001
2 49021 45.0037 329.0081 0008364 148.6137 211.5200 14.08555673 06
| Epoch (UTC): | 25 May 2026 14:31:55 |
| Eccentricity: | 0.0008364 |
| inclination: | 45.0037° |
| perigee height: | 858 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 329.0081° |
| argument of perigee: | 148.6137° |
| revolutions per day: | 14.08555673 |
| mean anomaly at epoch: | 211.5200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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