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 57601U 23118B 24055.25374977 -.00020955 00000-0 00000-0 0 9996
2 57601 41.4630 111.9766 9449526 206.0347 269.5618 0.10060724 132
| Epoch (UTC): | 24 February 2024 06:05:23 |
| Eccentricity: | 0.9449526 |
| inclination: | 41.4630° |
| perigee height: | 4371 km |
| apogee height: | 373420 km |
| right ascension of ascending node: | 111.9766° |
| argument of perigee: | 206.0347° |
| revolutions per day: | 0.10060724 |
| mean anomaly at epoch: | 269.5618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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