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 54653U 26145.56695509 +.00000000 +00000-0 -12426-3 0 00008
2 54653 87.9254 248.4959 0002124 97.2282 262.9093 13.21827329 09
| Epoch (UTC): | 25 May 2026 13:36:24 |
| Eccentricity: | 0.0002124 |
| inclination: | 87.9254° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4959° |
| argument of perigee: | 97.2282° |
| revolutions per day: | 13.21827329 |
| mean anomaly at epoch: | 262.9093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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