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 00573U 26110.06184455 +.00000000 +00000-0 +65624-3 0 00007
2 00573 42.7650 45.8974 4007693 80.2096 330.3891 6.39269023 09
| Epoch (UTC): | 20 April 2026 01:29:03 |
| Eccentricity: | 0.4007693 |
| inclination: | 42.7650° |
| perigee height: | 971 km |
| apogee height: | 10800 km |
| right ascension of ascending node: | 45.8974° |
| argument of perigee: | 80.2096° |
| revolutions per day: | 6.39269023 |
| mean anomaly at epoch: | 330.3891° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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