▸Orbital parameters

Orbit class	GEO
Inclination	4.3603°
Eccentricity	0.0003975
Period	1436.1 min
Apogee	35,803 km
Perigee	35,770 km
Mean motion	1.00271595 rev/day
RAAN	76.3345°
Arg of perigee	20.3777°
Mean anomaly	125.6563°
B*	0.0000e+0
Rev at epoch	4,665

▸Two-line element set (TLE)

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

1 28868U 05036A 26188.12381007 -.00000062 00000-0 00000-0 0 9992

2 28868 4.3603 76.3345 0003975 20.3777 125.6563 1.00271595 46657

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ANIK F1R",
  "OBJECT_ID": "2005-036A",
  "EPOCH": "2026-07-07T02:58:17.19+00:00",
  "MEAN_MOTION": 1.00271595,
  "ECCENTRICITY": 0.0003975,
  "INCLINATION": 4.3603,
  "RA_OF_ASC_NODE": 76.3345,
  "ARG_OF_PERICENTER": 20.3777,
  "MEAN_ANOMALY": 125.6563,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 28868,
  "REV_AT_EPOCH": 4665,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -6.2e-7,
  "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	ANIK F1R
Operator	Telesat CanadaHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Canada
Launch date	Sep 8, 2005HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4500HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/28868

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