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 37838U 11058A 23066.38423802 .00958156 32324-3 26800-2 0 9990
2 37838 19.9573 299.5316 0095894 286.8982 72.0723 15.84787083590138
| Epoch (UTC): | 07 March 2023 09:13:18 |
| Eccentricity: | 0.0095894 |
| inclination: | 19.9573° |
| perigee height: | 253 km |
| apogee height: | 381 km |
| right ascension of ascending node: | 299.5316° |
| argument of perigee: | 286.8982° |
| revolutions per day: | 15.84787083 |
| mean anomaly at epoch: | 72.0723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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