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 53504U 26145.66668980 +.00000000 +00000-0 +14473-1 0 00007
2 53504 97.6035 267.7445 0001378 78.0095 6.2525 15.44702559 04
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001378 |
| inclination: | 97.6035° |
| perigee height: | 431 km |
| apogee height: | 433 km |
| right ascension of ascending node: | 267.7445° |
| argument of perigee: | 78.0095° |
| revolutions per day: | 15.44702559 |
| mean anomaly at epoch: | 6.2525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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