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 68237U 26145.12221450 +.00000000 +00000-0 +12045-2 0 00008
2 68237 53.1601 295.4221 0002068 82.8261 277.2977 15.34437296 07
| Epoch (UTC): | 25 May 2026 02:55:59 |
| Eccentricity: | 0.0002068 |
| inclination: | 53.1601° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 295.4221° |
| argument of perigee: | 82.8261° |
| revolutions per day: | 15.34437296 |
| mean anomaly at epoch: | 277.2977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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