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 68067U 26145.45293898 +.00000000 +00000-0 +48300-3 0 00004
2 68067 53.1599 51.7267 0001449 94.3634 265.7534 15.34411290 08
| Epoch (UTC): | 25 May 2026 10:52:13 |
| Eccentricity: | 0.0001449 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 51.7267° |
| argument of perigee: | 94.3634° |
| revolutions per day: | 15.34411290 |
| mean anomaly at epoch: | 265.7534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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