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 49133U 26145.29598562 +.00000000 +00000-0 -26073-4 0 00000
2 49133 69.9993 101.3044 0003556 266.0713 94.0040 14.98335540 03
| Epoch (UTC): | 25 May 2026 07:06:13 |
| Eccentricity: | 0.0003556 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 101.3044° |
| argument of perigee: | 266.0713° |
| revolutions per day: | 14.98335540 |
| mean anomaly at epoch: | 94.0040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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