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 27840U 03031A 25138.89240474 .00000169 00000-0 64925-4 0 9991
2 27840 98.5814 111.8861 0098315 78.6528 282.5686 14.39677025149269
| Epoch (UTC): | 18 May 2025 21:25:03 |
| Eccentricity: | 0.0098315 |
| inclination: | 98.5814° |
| perigee height: | 689 km |
| apogee height: | 830 km |
| right ascension of ascending node: | 111.8861° |
| argument of perigee: | 78.6528° |
| revolutions per day: | 14.39677025 |
| mean anomaly at epoch: | 282.5686° |
| orbit number at epoch: | 14926 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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