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 27386U 02009A 25134.11693432 .00000124 00000-0 54056-4 0 9992
2 27386 98.3319 90.6548 0001208 90.5579 279.7980 14.38910552216165
| Epoch (UTC): | 14 May 2025 02:48:23 |
| Eccentricity: | 0.0001208 |
| inclination: | 98.3319° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 90.6548° |
| argument of perigee: | 90.5579° |
| revolutions per day: | 14.38910552 |
| mean anomaly at epoch: | 279.7980° |
| orbit number at epoch: | 21616 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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