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 60133U 26145.56882169 +.00000000 +00000-0 +00000-0 0 00009
2 60133 0.0161 86.2555 0000622 33.4358 253.0443 1.00270641 02
| Epoch (UTC): | 25 May 2026 13:39:06 |
| Eccentricity: | 0.0000622 |
| inclination: | 0.0161° |
| perigee height: | 35784 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 86.2555° |
| argument of perigee: | 33.4358° |
| revolutions per day: | 1.00270641 |
| mean anomaly at epoch: | 253.0443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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