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 54234U 26145.54987459 +.00000000 +00000-0 +37964-4 0 00003
2 54234 98.7054 84.7201 0000505 249.7104 110.4018 14.19560700 00
| Epoch (UTC): | 25 May 2026 13:11:49 |
| Eccentricity: | 0.0000505 |
| inclination: | 98.7054° |
| perigee height: | 826 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 84.7201° |
| argument of perigee: | 249.7104° |
| revolutions per day: | 14.19560700 |
| mean anomaly at epoch: | 110.4018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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