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 68180U 26144.70568962 +.00000000 +00000-0 +10915-2 0 00004
2 68180 53.1586 273.5166 0001187 57.6662 302.4457 15.38860087 03
| Epoch (UTC): | 24 May 2026 16:56:11 |
| Eccentricity: | 0.0001187 |
| inclination: | 53.1586° |
| perigee height: | 449 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 273.5166° |
| argument of perigee: | 57.6662° |
| revolutions per day: | 15.38860087 |
| mean anomaly at epoch: | 302.4457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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