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 data is extracted from the following two-line orbital elements,
1 39026U 12072A 22179.00696897 .00009266 00000-0 25439-3 0 9997
2 39026 97.2671 169.6076 0032399 119.4644 240.9840 15.36924218530606
| Epoch (UTC): | 28 June 2022 00:10:02 |
| Eccentricity: | 0.0032399 |
| inclination: | 97.2671° |
| perigee height: | 433 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 169.6076° |
| argument of perigee: | 119.4644° |
| revolutions per day: | 15.36924218 |
| mean anomaly at epoch: | 240.9840° |
| orbit number at epoch: | 53060 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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