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 68959U 26145.58335647 +.00000000 +00000-0 +40307-3 0 00006
2 68959 53.1587 268.7854 0001394 49.7661 61.3394 15.49311344 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001394 |
| inclination: | 53.1587° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 268.7854° |
| argument of perigee: | 49.7661° |
| revolutions per day: | 15.49311344 |
| mean anomaly at epoch: | 61.3394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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