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 27561U 02054C 23153.52904222 .00000502 00000-0 12251-3 0 9993
2 27561 98.5261 333.6402 0044699 312.3761 47.3656 14.56567368 88873
| Epoch (UTC): | 02 June 2023 12:41:49 |
| Eccentricity: | 0.0044699 |
| inclination: | 98.5261° |
| perigee height: | 672 km |
| apogee height: | 736 km |
| right ascension of ascending node: | 333.6402° |
| argument of perigee: | 312.3761° |
| revolutions per day: | 14.56567368 |
| mean anomaly at epoch: | 47.3656° |
| orbit number at epoch: | 8887 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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