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 36453U 26102.25731741 +.00000000 +00000-0 +60110-3 0 00006
2 36453 73.9199 283.3496 0070058 160.2787 19.4587 14.53644529 04
| Epoch (UTC): | 12 April 2026 06:10:32 |
| Eccentricity: | 0.0070058 |
| inclination: | 73.9199° |
| perigee height: | 664 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 283.3496° |
| argument of perigee: | 160.2787° |
| revolutions per day: | 14.53644529 |
| mean anomaly at epoch: | 19.4587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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