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 00005U 26129.92706125 +.00000000 +00000-0 +16962-3 0 00007
2 00005 34.2511 72.4006 1836382 325.9545 23.5494 10.85980204 00
| Epoch (UTC): | 09 May 2026 22:14:58 |
| Eccentricity: | 0.1836382 |
| inclination: | 34.2511° |
| perigee height: | 654 km |
| apogee height: | 3817 km |
| right ascension of ascending node: | 72.4006° |
| argument of perigee: | 325.9545° |
| revolutions per day: | 10.85980204 |
| mean anomaly at epoch: | 23.5494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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