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 25341.28760825 .00002664 00000-0 42317-3 0 9990
2 27939 98.3367 155.3432 0011817 152.2009 332.6417 14.72947527187299
| Epoch (UTC): | 07 December 2025 06:54:09 |
| Eccentricity: | 0.0011817 |
| inclination: | 98.3367° |
| perigee height: | 643 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 155.3432° |
| argument of perigee: | 152.2009° |
| revolutions per day: | 14.72947527 |
| mean anomaly at epoch: | 332.6417° |
| orbit number at epoch: | 18729 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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