▸Orbital parameters

Orbit class	GEO
Inclination	0.2218°
Eccentricity	0.0001460
Period	1436.1 min
Apogee	35,793 km
Perigee	35,781 km
Mean motion	1.00270232 rev/day
RAAN	308.9798°
Arg of perigee	329.5843°
Mean anomaly	98.2432°
B*	0.0000e+0
Rev at epoch	132

▸Two-line element set (TLE)

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

1 67757U 26028B 26188.16017221 .00000171 00000-0 00000-0 0 9994

2 67757 0.2218 308.9798 0001460 329.5843 98.2432 1.00270232 1327

▸ source OMM (JSON)

{
  "OBJECT_NAME": "JAM-E JAM 1",
  "OBJECT_ID": "2026-028B",
  "EPOCH": "2026-07-07T03:50:38.879+00:00",
  "MEAN_MOTION": 1.00270232,
  "ECCENTRICITY": 0.000146,
  "INCLINATION": 0.2218,
  "RA_OF_ASC_NODE": 308.9798,
  "ARG_OF_PERICENTER": 329.5843,
  "MEAN_ANOMALY": 98.2432,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67757,
  "REV_AT_EPOCH": 132,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000171,
  "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	JAM-E JAM 1
Operator	Islamic Republic of Iran BroadcastingHIGHvia GCAT — Jonathan McDowell's General Catalog Islamic Republic of Iran BroadcastingMEDIUMvia Wikidata
Country	IranMEDIUMvia Wikidata
Launch date	Feb 12, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	150HIGH

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/67757

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