▸Orbital parameters

Orbit class	LEO
Inclination	64.5520°
Eccentricity	0.0074752
Period	97.1 min
Apogee	672 km
Perigee	567 km
Mean motion	14.83088031 rev/day
RAAN	67.3282°
Arg of perigee	258.7570°
Mean anomaly	100.5128°
B*	1.0582e-4
Rev at epoch	26,741

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 27607U 02058C 26188.11499616 .00000749 00000-0 10582-3 0 9998

2 27607 64.5520 67.3282 0074752 258.7570 100.5128 14.83088031267416

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SAUDISAT 1C (SO-50)",
  "OBJECT_ID": "2002-058C",
  "EPOCH": "2026-07-07T02:45:35.668+00:00",
  "MEAN_MOTION": 14.83088031,
  "ECCENTRICITY": 0.0074752,
  "INCLINATION": 64.552,
  "RA_OF_ASC_NODE": 67.3282,
  "ARG_OF_PERICENTER": 258.757,
  "MEAN_ANOMALY": 100.5128,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 27607,
  "REV_AT_EPOCH": 26741,
  "BSTAR": 0.00010582,
  "MEAN_MOTION_DOT": 0.00000749,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	SAUDISAT 1C (SO-50)
Operator	King Abdul Aziz City for Science and TechnologyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Saudi Arabia
Launch date	Dec 20, 2002HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	15HIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree 10MEDIUMvia Wikidata

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/27607

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.