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 53030U 26145.17920832 +.00000000 +00000-0 -16416-3 0 00006
2 53030 53.2133 100.9375 0001394 83.6512 276.4639 15.08841774 09
| Epoch (UTC): | 25 May 2026 04:18:03 |
| Eccentricity: | 0.0001394 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.9375° |
| argument of perigee: | 83.6512° |
| revolutions per day: | 15.08841774 |
| mean anomaly at epoch: | 276.4639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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