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 51133U 26145.17230553 +.00000000 +00000-0 +18435-3 0 00004
2 51133 53.2130 315.7768 0000912 97.2974 262.8122 15.08828243 00
| Epoch (UTC): | 25 May 2026 04:08:07 |
| Eccentricity: | 0.0000912 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 315.7768° |
| argument of perigee: | 97.2974° |
| revolutions per day: | 15.08828243 |
| mean anomaly at epoch: | 262.8122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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