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 27939U 03042A 23087.08720183 .00002534 00000-0 44924-3 0 9998
2 27939 98.2285 233.5107 0012910 37.5580 322.6472 14.68112387 42641
| Epoch (UTC): | 28 March 2023 02:05:34 |
| Eccentricity: | 0.0012910 |
| inclination: | 98.2285° |
| perigee height: | 658 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 233.5107° |
| argument of perigee: | 37.5580° |
| revolutions per day: | 14.68112387 |
| mean anomaly at epoch: | 322.6472° |
| orbit number at epoch: | 4264 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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