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 40053U 26145.64852465 +.00000000 +00000-0 +12509-3 0 00003
2 40053 98.0637 208.7200 0001216 80.5619 279.5719 14.60935689 06
| Epoch (UTC): | 25 May 2026 15:33:52 |
| Eccentricity: | 0.0001216 |
| inclination: | 98.0637° |
| perigee height: | 689 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 208.7200° |
| argument of perigee: | 80.5619° |
| revolutions per day: | 14.60935689 |
| mean anomaly at epoch: | 279.5719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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