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 53480U 26145.66668980 +.00000000 +00000-0 +40353-2 0 00007
2 53480 97.6023 268.5339 0001299 92.5885 241.5523 15.35430193 09
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001299 |
| inclination: | 97.6023° |
| perigee height: | 459 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 268.5339° |
| argument of perigee: | 92.5885° |
| revolutions per day: | 15.35430193 |
| mean anomaly at epoch: | 241.5523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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