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 54681U 26145.54004517 +.00000000 +00000-0 +25224-3 0 00009
2 54681 87.9254 248.4844 0001972 93.5055 266.6304 13.21827174 04
| Epoch (UTC): | 25 May 2026 12:57:39 |
| Eccentricity: | 0.0001972 |
| inclination: | 87.9254° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4844° |
| argument of perigee: | 93.5055° |
| revolutions per day: | 13.21827174 |
| mean anomaly at epoch: | 266.6304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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