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 41335U 26107.27369207 +.00000000 +00000-0 +48787-4 0 00009
2 41335 98.6282 175.5216 0001004 93.6838 266.4457 14.26736651 07
| Epoch (UTC): | 17 April 2026 06:34:06 |
| Eccentricity: | 0.0001004 |
| inclination: | 98.6282° |
| perigee height: | 802 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 175.5216° |
| argument of perigee: | 93.6838° |
| revolutions per day: | 14.26736651 |
| mean anomaly at epoch: | 266.4457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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