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 53471U 26145.58391247 +.00000000 +00000-0 -10978-3 0 00009
2 53471 97.4445 266.5936 0001871 103.6544 256.4892 15.05659603 08
| Epoch (UTC): | 25 May 2026 14:00:50 |
| Eccentricity: | 0.0001871 |
| inclination: | 97.4445° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 266.5936° |
| argument of perigee: | 103.6544° |
| revolutions per day: | 15.05659603 |
| mean anomaly at epoch: | 256.4892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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