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 54230U 26145.54476602 +.00000000 +00000-0 +00000-0 0 00009
2 54230 0.0155 14.0764 0002132 62.6565 165.7063 1.00272040 01
| Epoch (UTC): | 25 May 2026 13:04:27 |
| Eccentricity: | 0.0002132 |
| inclination: | 0.0155° |
| perigee height: | 35778 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 14.0764° |
| argument of perigee: | 62.6565° |
| revolutions per day: | 1.00272040 |
| mean anomaly at epoch: | 165.7063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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