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 54138U 26145.46062895 +.00000000 +00000-0 +18996-3 0 00008
2 54138 87.9159 309.4947 0001629 85.2028 274.9290 13.19726431 01
| Epoch (UTC): | 25 May 2026 11:03:18 |
| Eccentricity: | 0.0001629 |
| inclination: | 87.9159° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.4947° |
| argument of perigee: | 85.2028° |
| revolutions per day: | 13.19726431 |
| mean anomaly at epoch: | 274.9290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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