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 68280U 26145.19692115 +.00000000 +00000-0 +69374-3 0 00001
2 68280 53.1591 322.5153 0001283 90.8986 269.2164 15.34403237 07
| Epoch (UTC): | 25 May 2026 04:43:33 |
| Eccentricity: | 0.0001283 |
| inclination: | 53.1591° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 322.5153° |
| argument of perigee: | 90.8986° |
| revolutions per day: | 15.34403237 |
| mean anomaly at epoch: | 269.2164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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