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 68987U 26145.46852765 +.00000000 +00000-0 +14729-3 0 00008
2 68987 97.7363 43.3435 0001539 145.6033 214.5285 14.91725956 03
| Epoch (UTC): | 25 May 2026 11:14:40 |
| Eccentricity: | 0.0001539 |
| inclination: | 97.7363° |
| perigee height: | 591 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 43.3435° |
| argument of perigee: | 145.6033° |
| revolutions per day: | 14.91725956 |
| mean anomaly at epoch: | 214.5285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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