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 68053U 26145.46814872 +.00000000 +00000-0 +84880-3 0 00004
2 68053 53.1607 53.2232 0001313 90.0550 270.0601 15.30209521 04
| Epoch (UTC): | 25 May 2026 11:14:08 |
| Eccentricity: | 0.0001313 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 53.2232° |
| argument of perigee: | 90.0550° |
| revolutions per day: | 15.30209521 |
| mean anomaly at epoch: | 270.0601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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