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 68549U 26145.58864806 +.00000000 +00000-0 +59015-3 0 00001
2 68549 53.1612 5.0260 0001152 88.0632 272.0502 15.34410488 07
| Epoch (UTC): | 25 May 2026 14:07:39 |
| Eccentricity: | 0.0001152 |
| inclination: | 53.1612° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 5.0260° |
| argument of perigee: | 88.0632° |
| revolutions per day: | 15.34410488 |
| mean anomaly at epoch: | 272.0502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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