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 27370U 02004A 23109.72733825 .11076608 49524-5 91122-3 0 9993
2 27370 38.0117 211.4651 0005722 342.5643 146.3565 16.38643363174403
| Epoch (UTC): | 19 April 2023 17:27:22 |
| Eccentricity: | 0.0005722 |
| inclination: | 38.0117° |
| perigee height: | 165 km |
| apogee height: | 173 km |
| right ascension of ascending node: | 211.4651° |
| argument of perigee: | 342.5643° |
| revolutions per day: | 16.38643363 |
| mean anomaly at epoch: | 146.3565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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