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 53479U 26145.32916362 +.00000000 +00000-0 -72195-4 0 00000
2 53479 97.4453 266.4504 0002672 120.0312 240.1180 15.05654040 01
| Epoch (UTC): | 25 May 2026 07:53:59 |
| Eccentricity: | 0.0002672 |
| inclination: | 97.4453° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 266.4504° |
| argument of perigee: | 120.0312° |
| revolutions per day: | 15.05654040 |
| mean anomaly at epoch: | 240.1180° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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