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 54754U 26145.55161977 +.00000000 +00000-0 +13219-4 0 00007
2 54754 77.6111 65.8654 0000117 97.0424 263.0741 14.00171722 07
| Epoch (UTC): | 25 May 2026 13:14:19 |
| Eccentricity: | 0.0000117 |
| inclination: | 77.6111° |
| perigee height: | 893 km |
| apogee height: | 893 km |
| right ascension of ascending node: | 65.8654° |
| argument of perigee: | 97.0424° |
| revolutions per day: | 14.00171722 |
| mean anomaly at epoch: | 263.0741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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