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 45133U 26145.21530197 +.00000000 +00000-0 -31324-3 0 00002
2 45133 87.8864 40.8391 0001832 78.3443 281.7890 13.10376612 02
| Epoch (UTC): | 25 May 2026 05:10:02 |
| Eccentricity: | 0.0001832 |
| inclination: | 87.8864° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8391° |
| argument of perigee: | 78.3443° |
| revolutions per day: | 13.10376612 |
| mean anomaly at epoch: | 281.7890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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