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 53469U 26145.29870066 +.00000000 +00000-0 -74366-4 0 00007
2 53469 97.4474 266.3717 0001266 108.8442 251.2923 15.05658670 05
| Epoch (UTC): | 25 May 2026 07:10:07 |
| Eccentricity: | 0.0001266 |
| inclination: | 97.4474° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 266.3717° |
| argument of perigee: | 108.8442° |
| revolutions per day: | 15.05658670 |
| mean anomaly at epoch: | 251.2923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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