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 68043U 26145.15107300 +.00000000 +00000-0 +10204-2 0 00008
2 68043 53.1596 54.8044 0001207 80.9538 279.1599 15.30206518 03
| Epoch (UTC): | 25 May 2026 03:37:32 |
| Eccentricity: | 0.0001207 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 54.8044° |
| argument of perigee: | 80.9538° |
| revolutions per day: | 15.30206518 |
| mean anomaly at epoch: | 279.1599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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