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 53320U 26145.61767522 +.00000000 +00000-0 +82002-3 0 00005
2 53320 34.9961 298.6878 0001495 75.7084 284.3803 15.43565551 03
| Epoch (UTC): | 25 May 2026 14:49:27 |
| Eccentricity: | 0.0001495 |
| inclination: | 34.9961° |
| perigee height: | 435 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 298.6878° |
| argument of perigee: | 75.7084° |
| revolutions per day: | 15.43565551 |
| mean anomaly at epoch: | 284.3803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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