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 53152U 26145.66668980 +.00000000 +00000-0 +15889-2 0 00009
2 53152 53.2180 173.2340 0000992 56.9132 282.1904 15.35726356 02
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000992 |
| inclination: | 53.2180° |
| perigee height: | 458 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 173.2340° |
| argument of perigee: | 56.9132° |
| revolutions per day: | 15.35726356 |
| mean anomaly at epoch: | 282.1904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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