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 54678U 26145.53499506 +.00000000 +00000-0 +31386-3 0 00006
2 54678 87.9253 248.4958 0001973 102.5540 257.5815 13.21827340 07
| Epoch (UTC): | 25 May 2026 12:50:23 |
| Eccentricity: | 0.0001973 |
| inclination: | 87.9253° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4958° |
| argument of perigee: | 102.5540° |
| revolutions per day: | 13.21827340 |
| mean anomaly at epoch: | 257.5815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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