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 53346U 26145.59844727 +.00000000 +00000-0 +16714-3 0 00000
2 53346 97.3146 214.3470 0001146 249.2706 110.8408 15.21502351 03
| Epoch (UTC): | 25 May 2026 14:21:45 |
| Eccentricity: | 0.0001146 |
| inclination: | 97.3146° |
| perigee height: | 501 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 214.3470° |
| argument of perigee: | 249.2706° |
| revolutions per day: | 15.21502351 |
| mean anomaly at epoch: | 110.8408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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