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 55748U 26145.15980687 +.00000000 +00000-0 +50972-4 0 00001
2 55748 70.0009 51.6906 0003014 268.2278 91.8536 14.98331016 05
| Epoch (UTC): | 25 May 2026 03:50:07 |
| Eccentricity: | 0.0003014 |
| inclination: | 70.0009° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 51.6906° |
| argument of perigee: | 268.2278° |
| revolutions per day: | 14.98331016 |
| mean anomaly at epoch: | 91.8536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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