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 07363U 26088.07134976 +.00000000 +00000-0 +41464-4 0 00006
2 07363 81.2236 86.5529 0017483 5.2835 354.8511 14.00262217 06
| Epoch (UTC): | 29 March 2026 01:42:44 |
| Eccentricity: | 0.0017483 |
| inclination: | 81.2236° |
| perigee height: | 880 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 86.5529° |
| argument of perigee: | 5.2835° |
| revolutions per day: | 14.00262217 |
| mean anomaly at epoch: | 354.8511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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