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 54279U 26087.48370788 +.00000000 +00000-0 +29446-3 0 00006
2 54279 98.6184 102.5048 0137358 308.4241 50.4675 14.31553969 07
| Epoch (UTC): | 28 March 2026 11:36:32 |
| Eccentricity: | 0.0137358 |
| inclination: | 98.6184° |
| perigee height: | 688 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 102.5048° |
| argument of perigee: | 308.4241° |
| revolutions per day: | 14.31553969 |
| mean anomaly at epoch: | 50.4675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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