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 68971U 26145.58335647 +.00000000 +00000-0 -32715-1 0 00003
2 68971 53.1596 268.3026 0000993 83.8857 264.9623 15.54102760 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000993 |
| inclination: | 53.1596° |
| perigee height: | 404 km |
| apogee height: | 405 km |
| right ascension of ascending node: | 268.3026° |
| argument of perigee: | 83.8857° |
| revolutions per day: | 15.54102760 |
| mean anomaly at epoch: | 264.9623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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