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 60903U 26145.63888116 +.00000000 +00000-0 +11238-4 0 00009
2 60903 53.1595 111.6772 0001177 85.6519 274.4634 15.69707846 06
| Epoch (UTC): | 25 May 2026 15:19:59 |
| Eccentricity: | 0.0001177 |
| inclination: | 53.1595° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 111.6772° |
| argument of perigee: | 85.6519° |
| revolutions per day: | 15.69707846 |
| mean anomaly at epoch: | 274.4634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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