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 55300U 26145.53240282 +.00000000 +00000-0 +37929-4 0 00004
2 55300 70.0010 190.5412 0003896 266.7331 93.3383 14.98410732 07
| Epoch (UTC): | 25 May 2026 12:46:39 |
| Eccentricity: | 0.0003896 |
| inclination: | 70.0010° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 190.5412° |
| argument of perigee: | 266.7331° |
| revolutions per day: | 14.98410732 |
| mean anomaly at epoch: | 93.3383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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