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 68019U 26145.38100193 +.00000000 +00000-0 +30747-3 0 00004
2 68019 97.2846 94.3573 0001881 91.3110 268.8348 15.33444058 02
| Epoch (UTC): | 25 May 2026 09:08:38 |
| Eccentricity: | 0.0001881 |
| inclination: | 97.2846° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.3573° |
| argument of perigee: | 91.3110° |
| revolutions per day: | 15.33444058 |
| mean anomaly at epoch: | 268.8348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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