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 is defined by the following mean orbital elements,
1 64849U 26145.35507233 +.00000000 +00000-0 +18403-3 0 00009
2 64849 97.4511 0.7124 0001609 70.0839 290.0561 15.05658291 02
| Epoch (UTC): | 25 May 2026 08:31:18 |
| Eccentricity: | 0.0001609 |
| inclination: | 97.4511° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.7124° |
| argument of perigee: | 70.0839° |
| revolutions per day: | 15.05658291 |
| mean anomaly at epoch: | 290.0561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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