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 23152.08645531 .00000444 00000-0 10970-3 0 9999
2 27561 98.5261 332.1652 0044771 316.8923 42.8771 14.56565582 88744
| Epoch (UTC): | 01 June 2023 02:04:29 |
| Eccentricity: | 0.0044771 |
| inclination: | 98.5261° |
| perigee height: | 672 km |
| apogee height: | 736 km |
| right ascension of ascending node: | 332.1652° |
| argument of perigee: | 316.8923° |
| revolutions per day: | 14.56565582 |
| mean anomaly at epoch: | 42.8771° |
| orbit number at epoch: | 8874 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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